Hoogsalt moodne Tallinn Fashion Week / Jaanika Terasmaa : intervjueerinud Annely Martin

Index Scriptorium Estoniae

Terasmaa, Jaanika

2010-01-01

Tallinn Fashion Week kestab 7. novembrini. Üks moenädala korraldajaid Jaanika Terasmaa, sellest, mida moenädal pakub tavainimesele ja kui oluline on selline ettevõtmine moeloojatele, moenädala eesmärgist

Tallinn 2011 ... mitte ainult koorikonkurss / Aivar Leštšinski

Index Scriptorium Estoniae

Leštšinski, Aivar, 1958-

2011-01-01

Festivali avapäeval esitletud CD-komplektist "Läbilõige eesti koorimuusikast" ja mõtteid, et riigitelevisioonis võik olla koorimuusikat puudutav saade ning koorifestivali "Tallinn 2011" tulemused

Madalmaade nukunäitlejate paremik hiilgas Tallinn Treffil / Tiiu Laks

Index Scriptorium Estoniae

Laks, Tiiu, 1984-

2010-01-01

5.-8. juunini 2010 toimuvast rahvusvahelisest festivalist Tallinn Treff. Hollandi trupi DudaPaiva lavastusest "Needus". Nukunäitleja Neville Tranteri (Austraalia-Holland) lavastusest "Punch ja Judy Afganistanis". Stef Vettersi (Belgia) etendusest "Tema kõrgeausus Ottfriedi tundmatu maailm"

Euroopa kultuuripealinn Tallinn 2011 paneb PÖFF-ile õla alla

Index Scriptorium Estoniae

2011-01-01

15. Pimedate Ööde Filmifestivali ja Euroopa Kultuuripealinna Tallinn 2011 koostöös alguse saanud noortele animavallas tegutsevatele professionaalidele mõeldud koolitussarjast AnimaCampus, rahvusvahelise filmituru Black Market ja programmi "60 sekundit üksindust aastal Null" toetamisest

Tallinn soovib linnahalli Ameerika investoritega ikka edasi minna / Raimo Poom

Index Scriptorium Estoniae

Poom, Raimo

2010-01-01

Tallinna linnavalitsus ootab enne otsustamist, kas pikendada Tallinna linnahalli arendamiseks sõlmitud eellepingut Ameerika ettevõttega Tallinn Entertainment LLC, Ameerika investorite delegatsiooni visiiti Tallinna. Rahandusminister Jürgen Ligi vastusest Tallinna abilinnapea Taavi Aasa kirjale, milles oli ettepanek kaaluda võimalust anda riigi garantii linnahalli arendamise projektile

Euroopa kultuuripealik 2011 (Tallinn) lõpuks leitud / Mikko Fritze ; interv. Kaarel Tarand

Index Scriptorium Estoniae

Fritze, Mikko, 1963-

2007-01-01

Tallinn on Euroopa 2011. a. kultuuripealinn. Intervjuu korraldava sihtasutuse tegevjuhi Mikko Fritzega. Tegevusprogrammist, ka infrastruktuuri projektidest (linnateater, Kultuurikatel, rannapromenaad, lauluväljak, linnahall) jm. SA bürool on kavatsus kolida Kultuurikatlasse

Arvustus : Vello Paatsi. Eesti talurahva loodusteadusliku maailmapildi kujunemine rahvakooli kaudu (1803-1918). - Tallinn : TPÜ Kirjastus, 2003. 206 lk. / Jaan-Mati Punning

Index Scriptorium Estoniae

Punning, Jaan-Mati, 1940-2009

2003-01-01

Rets. rmt. : Paatsi, Vello. Eesti talurahva loodusteadusliku maailmapildi kujunemine rahvakooli kaudu (1803-1918). - Tallinn : Tallinna Pedagoogikaülikooli kirjastus, 2003. - 206 lk. : ill. - (Tallinna Pedagoogikaülikool. Sotsiaalteaduste dissertatsioonid = Tallinn Pedagogical University. Dissertations on social sciences, 1406-4405 ; 5)

"Tallinn Jazz Weekend" tõi kultuuripealinna Euroopa jazzielu korraldajad / Marje Ingel, Joosep Sang

Index Scriptorium Estoniae

Ingel, Marje

2011-01-01

Jazziorganisatsioonist Europe Jazz Network ja selle aastakonverentsist Tallinnas ning J. Sang selle raames Von Krahli teatris toimunud Tallinn Jazz Weekendi eesti jazzmuusika showcase-festivalist lühidalt

Siim Nestor soovitab : Tallinn Doom Night vol.1. Odessa Pop / Siim Nestor

Index Scriptorium Estoniae

Nestor, Siim, 1974-

2006-01-01

Soome doom-metal ansambel Reverend Bizarre üritusel "Tallinn Doom Night vol.1" 8. dets. klubis Rockstar's. Indipoppi viljelev Rootsi duo My Darling Yoy! üritusel "Odessa Pop" 9. dets. Tallinnas klubis KuKu

[Karin Hallas. Das Tallinner Mietshaus. Vom Historismus bis zum Jugendstil] / Paul Kaegbein

Index Scriptorium Estoniae

Kaegbein, Paul

2006-01-01

Arvustus: Karin Hallas. Das Tallinner Mietshaus. Vom Historismus bis zum Jugendstil. In: Architektur und bildende Kunst im Baltikum um 1900. Frankfurt am Main, Berlin, Bern, Bruxelles, New York, Wien: Lang 1999. S. 173-192.

A rapid situation assessment of the market for surrogate and illegal alcohols in Tallinn, Estonia.

Science.gov (United States)

Pärna, Kersti; Lang, Katrin; Raju, Kadi; Väli, Marika; McKee, Martin

2007-01-01

To understand the phenomenon of consumption of surrogate and illegal alcohols in Tallinn, capital of Estonia. This study, conducted in Tallinn in May 2006, used rapid situation assessment. Interviews with key informants in relevant settings such as emergency departments of hospitals, accommodation for the homeless, police etc. (n = 22), with alcohol abusers (n = 33), natural observations of surrogate sale and consumption venues (n = 46), and tracking of trade data were carried out. Key informants confirmed that consumption of illegal and surrogate alcohols are widely used by alcohol abusers, a finding confirmed by the alcohol abusers. Availability of surrogates varied by area of the city, mainly sold from street kiosks. Illegally produced spirits were also easily available. Sales of surrogates appear to have increased in recent years. A range of alcohol-containing substances that appear to be easily available at low cost, and that have high concentration of ethanol or contaminants known to be toxic, were identified in Tallinn. Alcohol policies in Estonia should address the consumption and availability of these substances.

Uhiuus orkester Tallinn Sinfonietta / Ivo Lille ja Risto Joost ; intervjueerinud Kristina Kõrver

Index Scriptorium Estoniae

Lille, Ivo, 1977-

2009-01-01

Kontserdiagentuurist HIMusic Agency ja Tallinn Sinfoniettast räägivad dirigent R. Joost ja I. Lille. Avakontserdist Vene Kultuurikeskuses, kus oli kavas Mozarti sümfooniad 1, 10 ja 40 ning kontsertaariad bulgaaria soprani Sonya Youncheva esituses

Tallinna Inglise kolledzhi spordihoone = The Tallinn English College's sports building

Index Scriptorium Estoniae

2008-01-01

Tallinna Inglise kolledzhi spordihoone (Estonia pst. 10, Tallinn) sisekujundusest. Arhitektid: Lembit-Kaur Stöör ja Margus Maiste (KOKO Arhitektid), sisearhitektid: Liisi Murula (Mari OÜ), Liis Lindvere ja Raili Paling, ornamentika: Martin Lazarev (KOKO Arhitektid). Sisearhitektidest, nende tähtsamad tööd. 5 korruse plaani, 2 värv. välis- ja 11 sisevaadet, fotod sisearhitektidest

Environmental innovation through transport policy. The implementation of the free fare policy on public transport in Tallinn, Estonia

Energy Technology Data Exchange (ETDEWEB)

Gabaldon-Estevan, D.

2016-07-01

Urban areas are of increasing relevance when it comes to sustainability: First, about half of the world’s population now lives in cities (increasing to 60% by 2030). Second, cities are nowadays responsible for levels of resource consumption and waste generation that are higher beyond their share on world population. Third, cities are more vulnerable to disruptive events that can lead to restrictions on the provision of resources and to changes on the environment caused by climate change. And fourth, because they concentrate key resources (political, social, cultural…), cities are seen as strategic scenarios where to experiment and develop solutions to cope with the prevailing sustainability challenges driven by the major social and environmental transformations. Urban agglomerations can be seen as complex innovation systems where human activities are shaped in order to transform societies towards sustainable development. For this paper, we focus on the case of an environmental innovation regarding transport policy, the implementation of the fare-free policy on public transport for all inhabitants of Tallinn, Estonia. Tallinn, with 414,000 inhabitants in 2015, is the capital of Estonia and the largest city in the country. Over the last two decades the share of public transport trips decreased dramatically. After a public opinion poll in 2012, in which over 75% of the participants voted for a fare-free public transportation system (FFPTS) in Tallinn, the new policy was implemented on 1st January 2013. From that date on inhabitants of Tallinn could use all public transport services (busses, trams, trolly-busses) operated by city-run operators for free. Later the fare-free system was implemented also on trains within Tallinn. In this paper we analyze the context, in which this policy was implemented, the main characteristics of its implementation and its actual situation. (Author)

[Lea Kõiv. Paul Johansen und das Stadtarchiv Reval/Tallinn] / Paul Kaegbein

Index Scriptorium Estoniae

Kaegbein, Paul

2008-01-01

Arvustus: Lea Kõiv. Paul Johansen und das Stadtarchiv Reval/Tallinn. - Nordosteuropa als Geschichtsregion. Helsinki : Aue-Stiftung; Lübeck : Schmict-Röhmild, 2006. Lk. 45-59. Artiklis on kasutatud seni avalikkusele vähetuntud materjale ja osaliselt käsitletud avalikke vaidlusi, kuhu olid segatud nii Paul Johansen kui järgmine linnaarhivaar Rudolf Kenkmaa

Programming Basics for Beginners. Experience of the Institute of Informatics at Tallinn University of Technology

Directory of Open Access Journals (Sweden)

Olga Mironova

2017-11-01

Full Text Available The present paper demonstrates the teaching approach in programming basics course for novices: schoolchildren of different ages and schoolteachers. This programming course was developed at the Institute of Informatics at Tallinn University of Technology in Tallinn, Estonia and it based on many years experience in teaching programming for non-IT first year students. The main aim of the chosen teaching approach in the course is to raise the motivation and keep the learners’ interest in programming field on the high level. The idea of developed teaching technique is the implementation of the visual programming before a serious textual coding. Furthermore, authors suggest readers some ways and methods to overcome learners’ difficulties in the first stage in a textual coding.

Püha Siimeoni ja Naisprohvet Hanna kiriku restaureerimine : Ahtri 5, Tallinn = Restoration of the Church of Righteous Symeon and Prophetess Ann : Ahtri 5, Tallinn / Epp Lankots

Index Scriptorium Estoniae

Lankots, Epp, 1976-

2005-01-01

18. sajandil ehitatud, 2001. a. Eesti Apostlik-Õigeusu Kirikule tagastatud kirikuhoone restaureerimine. Ees on interjööride konserveerimistööd. Uuringud: Juhan Kilumets, Eva Mölder. Arhitektuurne projekt: Tõnu Parmakson, Ilmar Kannelmäe. Konstruktiivne projekt: Aleksander Danil. Teostus: J. Kilumets (Rändmeister), T. Parmakson (Frantsiskus), E. Mölder (Vana Tallinn). Ill.: 3 värv. välis- ja 3 sisevaadet

Verifying Architectural Design Rules of the Flight Software Product Line

Science.gov (United States)

Ganesan, Dharmalingam; Lindvall, Mikael; Ackermann, Chris; McComas, David; Bartholomew, Maureen

2009-01-01

This paper presents experiences of verifying architectural design rules of the NASA Core Flight Software (CFS) product line implementation. The goal of the verification is to check whether the implementation is consistent with the CFS architectural rules derived from the developer's guide. The results indicate that consistency checking helps a) identifying architecturally significant deviations that were eluded during code reviews, b) clarifying the design rules to the team, and c) assessing the overall implementation quality. Furthermore, it helps connecting business goals to architectural principles, and to the implementation. This paper is the first step in the definition of a method for analyzing and evaluating product line implementations from an architecture-centric perspective.

Tallinn Fashion Week täidab nädala kodumaise moega / Karilin Engelbrecht

Index Scriptorium Estoniae

Engelbrecht, Karilin

2009-01-01

Tallinn Fashion Week'i üritustest. Ülevaade eesti moekunstnike loomingu esitlustest. Näitus "Uus Eesti moejoonistus" Arhitektuuri- ja Disainigaleriis. Anu Hindi moefotonäitus "Aeg maha 3" Iida galeriis. Raamatu "Eesti moepiibel 2010" esitlus Rotermanni kvartali kohvikus Platz. Oksana Tanditi ja Filippo Caroti moefotonäitus "Butterflies" Tallinna botaanikaaias

Development of Small UAS Beyond-Visual-Line-of-Sight (BVLOS Flight Operations: System Requirements and Procedures

Directory of Open Access Journals (Sweden)

Scott Xiang Fang

2018-04-01

Full Text Available Due to safety concerns of integrating small unmanned aircraft systems (UAS into non-segregated airspace, aviation authorities have required a set of detect and avoid (DAA systems to be equipped on small UAS for beyond-visual-line-of-sight (BVLOS flight operations in civil airspace. However, the development of small UAS DAA systems also requires BVLOS flights for testing and validation. To mitigate operational risks for small UAS BVLOS flight operations, this paper proposes to initially test small UAS DAA systems in BVLOS flights in a restricted airspace with additional safety features. Later, this paper further discusses the operating procedures and emergency action plans for small UAS BVLOS flight operations. The testing results show that these safety systems developed can help improve operational safety for small UAS BVLOS flight operations.

Stitch and hem and line and flight

Science.gov (United States)

Thorp, John Daniel

Stitch and hem and line and flight appears in four formats. There is this present one, which adheres to the manuscript design requirements as outlined by The Graduate School at The University of Utah; there is another which is a book six inches high by nine inches wide, printed in three colors, with text aligned to its gutter; and there is a broadside printed from the same forms of standing metal type on a single twelve-inch-high by nineteen-inch-wide page, where all spreads are registered to the same points so that all lines of all sections overlap exactly, excluding the last lines of the longest section, which are left immediately readable. The second and the third formats were produced in editions of fifty each, and copies are available to the reader through the Special Collections Library at the J. Willard Marriott Library. The text in the book you're holding is built from scans taken from the original letterpress pages, and so honors typos not caught before production during proofreading, but does not honor the final runs of production which overprint eight typos and overprint one duplicated "no." The text here stands as an uncorrected and reformatted transcript of the letterpress-printed pages, since all "characters must be clear and sharp. Smudged, indistinct, or blurred letters are not acceptable." The present format cannot ask (at least not in the same way) if the techniques and repetitive labor of hand printing can be read just as one might read any of the other more familiar small crises in a work: the line break, the influence of a culture or history on that work, anagnorisis, exegesis, etc. The present format doesn't seem to ask questions like: what happens to a love song when you can't read it or hear it? How does a line or letter make itself mean when cast in metal, stood up and pressed onto paper? Still, the present format is concerned with how a line sits on a page and how a line is like love is like highs is like sand. The text all these formats

Bob Scott: Tallinn 2011 saab oma preemiaraha kätte / Bob Scott ; intervjueerinud Teele Tammeorg

Index Scriptorium Estoniae

Scott, Bob

2010-01-01

Euroopa kultuuripealinnade hindamiskomisjoni esimees räägib oma kohtumisest Tallinna linnapea Edgar Savisaare ja kultuuriministri Laine Jänesega ning sellest, et Tallinnal ja Eestil tuleb lisatoetuse saamiseks saata Euroopa Komisjonile vaid kiri, milles nad kinnitavad, et kultuuripealinna programmi jaoks on raha olemas

"Tallinn Treff" - maailma lavade uus põlvkond Tallinnas / Meelis Pai, Vahur Keller, Reeda Toots ; intervjueerinud Margot Visnap

Index Scriptorium Estoniae

Pai, Meelis, 1968-

2009-01-01

30. maist 6. juunini toimuvast rahvusvahelisest nukuteatrifestivalist "Tallinn Treff" ning selle alafestivalist "Noor vaim" annavad ülevaate festivali peakorraldaja Meelis Pai, kusntiline juht Vahut Keller ja "Noor vaimu" juht Reeda Toots

Characteristics of cardiovascular deaths in forensic medical cases in Budapest, Vilnius and Tallinn.

Science.gov (United States)

Törő, Klara; Väli, Marika; Lepik, Delia; Tuusov, Jana; Dunay, György; Marcsa, Boglarka; Pauliukevicius, Alvydas; Raudys, Romas; Caplinskiene, Marija

2013-11-01

Evaluation of the pathomorphological characteristics of cases involving natural and sudden cardiovascular death is essential for the determination of the cause of death. The main purpose of this study is to investigate sudden unexpected cardiovascular death and to study how different geographical climatic influences may affect cardiac mortality in three capitals: Budapest, Vilnius and Tallinn. There were 8482 (5753 male, 2729 female) cardiovascular deaths between 2005 and 2009. The highest rate was observed in the age group between 71 and 80 years (35.17%) and 51-60 years (24.45%). The highest number of cardiovascular deaths occur in January (805/9.49%) and December (770/9.07%). Seasonal distribution was observed, with winter prevalence in Tallinn (279/3.20%) and spring prevalence in Vilnius (760/8.90%). Though in Vilnius and Budapest a great number of deaths occurred in winter and spring, any correlation with other factors (e.g. age, gender, BAC) was not statistically significant. Based on our results we can conclude that environmental-geographical parameters may affect natural cardiovascular death. Examination of pathological patterns and predisposing environmental parameters may help to improve prevention strategies. Copyright © 2013. Published by Elsevier Ltd.

Flight route Designing and mission planning Of power line inspecting system Based On multi-sensor UAV

International Nuclear Information System (INIS)

Xiaowei, Xie; Zhengjun, Liu; Zhiquan, Zuo

2014-01-01

In order to obtain various information of power facilities such as spatial location, geometry, images data and video information in the infrared and ultraviolet band and so on, Unmanned Aerial Vehicle (UAV) power line inspecting system needs to integrate a variety of sensors for data collection. Low altitude and side-looking imaging are required for UAV flight to ensure sensors to acquire high-quality data and device security. In this paper, UAV power line inspecting system is deferent from existing ones that used in Surveying and Mapping. According to characteristics of UAV for example equipped multiple sensor, side-looking imaging, working at low altitude, complex terrain conditions and corridor type flight, this paper puts forward a UAV power line inspecting scheme which comprehensively considered of the UAV performance, sensor parameters and task requirements. The scheme is finally tested in a region of Guangdong province, and the preliminary results show that the scheme is feasible

In-Flight Spectral Calibration of the APEX Imaging Spectrometer Using Fraunhofer Lines

Science.gov (United States)

Kuhlmann, Gerrit; Hueni, Andreas; Damm, Aalexander; Brunner, Dominik

2015-11-01

The Airborne Prism EXperiment (APEX) is an imaging spectrometer which allows to observe atmospheric trace gases such as nitrogen dioxide (NO2). Using a high resolution spectrum of solar Fraunhofer lines, APEX measurements collected during flight have been spectrally calibrated for centre wavelength positions (CW) and instrument slit function (ISF) and compared to the laboratory calibration. We find that CWs depend strongly on both across- and along-track position due to spectral smile and CWs dependency on ambient pressure. The width of the ISF is larger than estimated from the laboratory calibration but can be described by a linear scaling of the laboratory values. The ISF width depends on across- but not on along-track direction. The results demonstrate the importance of characterizing and monitoring the instrument performance during flight and will be used to improve the Empa APEX NO2 retrieval algorithm.

Uudised : Preemia "edition 49" noodigraafikale. Noor muusik ئ Tallinn 2000. Bergenisse sõidab Bezrodnaja / Hugo Alter

Index Scriptorium Estoniae

Alter, Hugo-Eduard, 1929-2003

2000-01-01

Kirjastuse "Edition 49" noodigraafikaga teos võitis muusikakirjastuspreemia "Frankfurt 2000". 6.-9. juunini toimub rahvusvaheline konkurss "Noor muusik ئ Tallinn 2000", millest võtavad osa kuni 13 aastased muusikud 11-st riigist. "Klassika-Eurovisiooni" Eesti võistluse finaali võitis A.-L. Bezrodnaja, kes esindab Eestit võistluse Euroopa finaalis juunis Bergenis

[Heinz von zur Mühlen. Paul Johansen und die Sogenannten Undeutschen in Reval/Tallinn] / Paul Kaegbein

Index Scriptorium Estoniae

Kaegbein, Paul

2008-01-01

Arvustus: Heinz von zur Mühlen. Paul Johansen und die Sogenannten Undeutschen in Reval/Tallinn. - Nordosteuropa als Geschichtsregion. Helsinki : Aue-Stiftung :; Lübeck : Schmidt-Römhild, 2006. lk. 103-111. Paul Johanseni lähim töökaaslane kirjeldab teose "Deutsch und Undeutsch im mittelalterlichen und frühneuzeitlichen Reval" valmimist

System Architecture of Small Unmanned Aerial System for Flight Beyond Visual Line-of-Sight

Science.gov (United States)

2015-09-17

International Conference on Mechatronic and Embedded Systems and Applications (MESA 2011), 28-31 (August 2011) Maddalon Jeffrey M., Kelly J... SYSTEM ARCHITECTURE OF SMALL UNMANNED AERIAL SYSTEM FOR FLIGHT BEYOND VISUAL LINE-OF-SIGHT THESIS...is declared a work of the U.S. Government and is not subject to copyright protection in the United States. AFIT-ENV-MS-15-S-047 SYSTEM

On-line control of the plasma spraying process by monitoring the temperature, velocity, and trajectory of in-flight particles

International Nuclear Information System (INIS)

Moreau, C.; Gougeon, P.; Lamontagne, M.; Lacasse, V.; Vaudreuil, G.; Cielo, P.

1994-01-01

This paper describes a new optical sensing device for on-line monitoring of the temperature, velocity and trajectory of in-flight particles during industrial coating production. Thermal radiation emitted by the in-flight particles is collected by a small and robust sensing head that can be attached to the plasma gun providing continuous monitoring of the spray process. The collected radiation is transmitted through optical fibers to a detection cabinet located away from the dusty environment around the operating plasma gun. On-line measurement of the particle velocity, temperature and trajectory can provide an efficient diagnostic tool to maintain optimum spraying conditions leading to a better reproducibility of the coating properties

M2-F1 in flight over lakebed on tow line

Science.gov (United States)

1963-01-01

After initial ground-tow flights of the M2-F1 using the Pontiac as a tow vehicle, the way was clear to make air tows behind a C-47. The first air tow took place on 16 August 1963. Pilot Milt Thompson found that the M2-F1 flew well, with good control. This first flight lasted less than two minutes from tow-line release to touchdown. The descent rate was 4,000 feet per minute. The wingless, lifting body aircraft design was initially concieved as a means of landing an aircraft horizontally after atmospheric reentry. The absence of wings would make the extreme heat of re-entry less damaging to the vehicle. In 1962, Dryden management approved a program to build a lightweight, unpowered lifting body as a prototype to flight test the wingless concept. It would look like a 'flying bathtub,' and was designated the M2-F1, the 'M' referring to 'manned' and 'F' referring to 'flight' version. It featured a plywood shell placed over a tubular steel frame crafted at Dryden. Construction was completed in 1963. The first flight tests of the M2-F1 were over Rogers Dry Lake at the end of a tow rope attached to a hopped-up Pontiac convertible driven at speeds up to about 120 mph. This vehicle needed to be able to tow the M2-F1 on the Rogers Dry Lakebed adjacent to NASA's Flight Research Center (FRC) at a minimum speed of 100 miles per hour. To do that, it had to handle the 400-pound pull of the M2-F1. Walter 'Whitey' Whiteside, who was a retired Air Force maintenance officer working in the FRC's Flight Operations Division, was a dirt-bike rider and hot-rodder. Together with Boyden 'Bud' Bearce in the Procurement and Supply Branch of the FRC, Whitey acquired a Pontiac Catalina convertible with the largest engine available. He took the car to Bill Straup's renowned hot-rod shop near Long Beach for modification. With a special gearbox and racing slicks, the Pontiac could tow the 1,000-pound M2-F1 110 miles per hour in 30 seconds. It proved adequate for the roughly 400 car tows that got

Flight Planning in the Cloud

Science.gov (United States)

Flores, Sarah L.; Chapman, Bruce D.; Tung, Waye W.; Zheng, Yang

2011-01-01

This new interface will enable Principal Investigators (PIs), as well as UAVSAR (Uninhabited Aerial Vehicle Synthetic Aperture Radar) members to do their own flight planning and time estimation without having to request flight lines through the science coordinator. It uses an all-in-one Google Maps interface, a JPL hosted database, and PI flight requirements to design an airborne flight plan. The application will enable users to see their own flight plan being constructed interactively through a map interface, and then the flight planning software will generate all the files necessary for the flight. Afterward, the UAVSAR team can then complete the flight request, including calendaring and supplying requisite flight request files in the expected format for processing by NASA s airborne science program. Some of the main features of the interface include drawing flight lines on the map, nudging them, adding them to the current flight plan, and reordering them. The user can also search and select takeoff, landing, and intermediate airports. As the flight plan is constructed, all of its components are constantly being saved to the database, and the estimated flight times are updated. Another feature is the ability to import flight lines from previously saved flight plans. One of the main motivations was to make this Web application as simple and intuitive as possible, while also being dynamic and robust. This Web application can easily be extended to support other airborne instruments.

A Quasi-Steady Lifting Line Theory for Insect-Like Hovering Flight.

Directory of Open Access Journals (Sweden)

Mostafa R A Nabawy

Full Text Available A novel lifting line formulation is presented for the quasi-steady aerodynamic evaluation of insect-like wings in hovering flight. The approach allows accurate estimation of aerodynamic forces from geometry and kinematic information alone and provides for the first time quantitative information on the relative contribution of induced and profile drag associated with lift production for insect-like wings in hover. The main adaptation to the existing lifting line theory is the use of an equivalent angle of attack, which enables capture of the steady non-linear aerodynamics at high angles of attack. A simple methodology to include non-ideal induced effects due to wake periodicity and effective actuator disc area within the lifting line theory is included in the model. Low Reynolds number effects as well as the edge velocity correction required to account for different wing planform shapes are incorporated through appropriate modification of the wing section lift curve slope. The model has been successfully validated against measurements from revolving wing experiments and high order computational fluid dynamics simulations. Model predicted mean lift to weight ratio results have an average error of 4% compared to values from computational fluid dynamics for eight different insect cases. Application of an unmodified linear lifting line approach leads on average to a 60% overestimation in the mean lift force required for weight support, with most of the discrepancy due to use of linear aerodynamics. It is shown that on average for the eight insects considered, the induced drag contributes 22% of the total drag based on the mean cycle values and 29% of the total drag based on the mid half-stroke values.

Russification of non-Estonian pupils in Tallinn

Directory of Open Access Journals (Sweden)

Ülle Rannut

2010-05-01

Full Text Available In the article home languages, their qualities and use by pupils in grades 2 to 5 in Tallinn are analyzed. Two larger and more characteristic groups (Ukrainians and Belarusians and two groups with Islamic backgrounds (Azerbaijanis and Tatars were compared with the aim of analysing different language loss and preservation factors. Although Ukrainians and Belarusians form much larger ethnic groups within Estonia, they have not managed to preserve their language anywhere near as successfully as the Azerbaijanis and Tatars. Comparison of the data suggests that language preservation in Estonia and the ability to withstand Russification are most influenced by the degree of difference of the language from Russian and the religious difference from the Russian Orthodox faith (and Soviet era atheism. Home languages are characterised by their use mainly in the verbal form, with skills in the literary language generally low or even non-existent. Languages are for the most part learned informally, primarily through communication with parents and/or grandparents. The result is a supersaturated vernacular with a large degree of variation and loans from superstratum languages which falls far from the standard of the language in question.DOI: http://dx.doi.org/10.5128/ERYa6.15

Punanahklusest: Majakovskist indiaanlasteni / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

2011-01-01

Tutvustus: Jangfeldt, Bengt. Mäng elu peale : Vladimir Majakovski ja tema lähikond / tõlkinud Anu Saluäär. Tallinn : Varrak, 2011 ; Céline, Louis-Ferdinand. Reis öö lõppu / tõlkinud Heli Allik. Tallinn : Varrak, 2010 ; Simone, Claude. Flandria tee / tõlkinud Leena Tomasberg. Tallinn : Eesti Raamat, 2011 ; Härm, Tiiu. Jää voolab : Eesti polaarränduri August Masiku maailm. Tallinn : Eesti Raamat, 2010 ; Page, Jake. Suure vaimu rüpes : Ameerika indiaanlaste 20 000-aastane ajalugu / tõlkinud Matti Piirimaa. Tallinn : Tänapäev, 2011

Flight Test Evaluation of an Unmanned Aircraft System Traffic Management (UTM) Concept for Multiple Beyond-Visual-Line-of-Sight Operations

Science.gov (United States)

Johnson, Marcus; Jung, Jaewoo; Rios, Joseph; Mercer, Joey; Homola, Jeffrey; Prevot, Thomas; Mulfinger, Daniel; Kopardekar, Parimal

2017-01-01

This study evaluates a traffic management concept designed to enable simultaneous operations of multiple small unmanned aircraft systems (UAS) in the national airspace system (NAS). A five-day flight-test activity is described that examined the feasibility of operating multiple UAS beyond visual line of sight (BVLOS) of their respective operators in the same airspace. Over the five-day campaign, three groups of five flight crews operated a total of eleven different aircraft. Each group participated in four flight scenarios involving five simultaneous missions. Each vehicle was operated BVLOS up to 1.5 miles from the pilot in command. Findings and recommendations are presented to support the feasibility and safety of routine BVLOS operations for small UAS.

Retsensioon : Riigikogu VII, VIII ja IX koosseis. Statistikat ja kommentaare. Peatoimetaja Aaro Mõttus. Tallinn : Riigikogu Kantselei, Eesti Rahvusraamatukogu, 2004. 326 lk. / Mart Nutt

Index Scriptorium Estoniae

Nutt, Mart, 1962-

2004-01-01

Arvustus: Riigikogu VII, VIII ja IX koosseis. Statistikat ja kommentaare / peatoim. Aaro Mõttus. Tallinn : Riigikogu Kantselei, Eesti Rahvusraamatukogu, 2004. - Lisatud: Ott Heinapuu tutvustav sõnum retsenseeritud väljaande kohta lk. 193. - Vt. ka: http://www.riigikogu.ee/rito/index.php?id=11357

From the Bronx to Bengifunda (and Other Lines of Flight): Deterritorializing Purposes and Methods in Science Education Research

Science.gov (United States)

Gough, Noel

2011-01-01

In this essay I explore a number of questions about purposes and methods in science education research prompted by my reading of Wesley Pitts' ethnographic study of interactions among four students and their teacher in a chemistry classroom in the Bronx, New York City. I commence three "lines of flight" (small acts of Deleuzo-Guattarian…

Flight Test Evaluation of an Unmanned Aircraft System Traffic Management (UTM) Concept for Multiple Beyond-Visual-Line-of-Sight (BVLOS) Operations

Science.gov (United States)

Johnson, Marcus; Jung, Jaewoo; Rios, Joseph; Mercer, Joey; Homola, Jeffrey; Prevot, Thomas; Mulfinger, Daniel; Kopardekar, Parimal

2017-01-01

This study evaluates a traffic management concept designed to enable simultaneous operations of multiple small unmanned aircraft systems (UAS) in the national airspace system (NAS). A five-day flight-test activity is described that examined the feasibility of operating multiple UAS beyond visual line of sight (BVLOS) of their respective operators in the same airspace. Over the five-day campaign, three groups of five flight crews operated a total of eleven different aircraft. Each group participated in four flight scenarios involving five simultaneous missions. Each vehicle was operated BVLOS up to 1.5 miles from the pilot in command. Findings and recommendations are presented to support the feasibility and safety of routine BVLOS operations for small UAS.

Transforming Image-Objects into Multiscale Fields: A GEOBIA Approach to Mitigate Urban Microclimatic Variability within H-Res Thermal Infrared Airborne Flight-Lines

Directory of Open Access Journals (Sweden)

Mir Mustafizur Rahman

2014-10-01

Full Text Available In an effort to minimize complex urban microclimatic variability within high-resolution (H-Res airborne thermal infrared (TIR flight-lines, we describe the Thermal Urban Road Normalization (TURN algorithm, which is based on the idea of pseudo invariant features. By assuming a homogeneous road temperature within a TIR scene, we hypothesize that any variation observed in road temperature is the effect of local microclimatic variability. To model microclimatic variability, we define a road-object class (Road, compute the within-Road temperature variability, sample it at different spatial intervals (i.e., 10, 20, 50, and 100 m then interpolate samples over each flight-line to create an object-weighted variable temperature field (a TURN-surface. The optimal TURN-surface is then subtracted from the original TIR image, essentially creating a microclimate-free scene. Results at different sampling intervals are assessed based on their: (i ability to visually and statistically reduce overall scene variability and (ii computation speed. TURN is evaluated on three non-adjacent TABI-1800 flight-lines (~182 km2 that were acquired in 2012 at night over The City of Calgary, Alberta, Canada. TURN also meets a recent GEOBIA (Geospatial Object Based Image Analysis challenge by incorporating existing GIS vector objects within the GEOBIA workflow, rather than relying exclusively on segmentation methods.

Poor weather conditions and flight operations: Implications for air ...

African Journals Online (AJOL)

This paper examined various weather hazards which include thunderstorm, fog, dust haze and line squall that affect flight operation such as flight delays, diversion and cancellation. The study revealed that fog accounted for 13.2% of flight cancellation at the airport and line squall similarly accounted for 10.1% of delays, ...

Data Envelopment Analysis of Helsinki-Tallinn Transportation Chains

Directory of Open Access Journals (Sweden)

Olli-Pekka Hilmola

2013-12-01

Full Text Available The Baltic Sea shipping is at a crossroads as sulphur regulation will lead to excessive cost increases from the year 2015 onwards and CO2 emission trading is planned to be implemented for the entire shipping sector within the EU area. Therefore, shipping is going to be minimized and hinterland transportation (road and rail will act as substitute. This research analyzes the situation on one of the highest volume general cargo transportation routes of Finland (operating between Helsinki, Finland and Tallinn, Estonia, including loading and unloading at seaports and short sea shipping activity in between. Based on the efficiency evaluation results, it seems that containers should be favoured over semi-trailers – containers could be carried efficiently either in container ships or even at currently favoured RoRo or RoPax ships. Our research illustrates that pure container shipping with larger container ships within the analyzed route is not entirely out of question, but lead time and hinterland operations should receive more attention. Alternatively, RoRo and RoPax ships can also do something to increase their competitiveness in environmental harm caused and diesel consumption – higher cargo loads and utilization levels are short-term key for continued dominance.

Numerical study of Tallinn storm-water system flooding conditions using CFD simulations of multi-phase flow in a large-scale inverted siphon

Science.gov (United States)

Kaur, K.; Laanearu, J.; Annus, I.

2017-10-01

The numerical experiments are carried out for qualitative and quantitative interpretation of a multi-phase flow processes associated with malfunctioning of the Tallinn storm-water system during rain storms. The investigations are focused on the single-line inverted siphon, which is used as under-road connection of pipes of the storm-water system under interest. A multi-phase flow solver of Computational Fluid Dynamics software OpenFOAM is used for simulating the three-phase flow dynamics in the hydraulic system. The CFD simulations are performed with different inflow rates under same initial conditions. The computational results are compared essentially in two cases 1) design flow rate and 2) larger flow rate, for emptying the initially filled inverted siphon from a slurry-fluid. The larger flow-rate situations are under particular interest to detected possible flooding. In this regard, it is anticipated that the CFD solutions provide an important insight to functioning of inverted siphon under a restricted water-flow conditions at simultaneous presence of air and slurry-fluid.

Simple flight time calibration generator in PLL technique

International Nuclear Information System (INIS)

Lauch, J.

1975-01-01

Calibration and routine check-ups of flight time measuring systems can be carried out with the aid of defined flight time calibration spectra. This paper describes a simple flight time calibration generator capable of generating such calibration spectra in the form of line spectra or of a white spectrum. The flight time of the generator is adjustable in steps from 100 to 3,200 ns. The number of calibration lines can be set to 10 or to 20, resulting in line spacings ranging from 5 to 320 ns. The stop signals are generated by a crystal oscillator, the start signals are generated by a voltage-controlled oscillator locked in a phase control circuit. The start and stop rates can be adjusted in steps. (orig.) [de

Cytological changes of root tip cells of alfalfa seeds after space flight

International Nuclear Information System (INIS)

Ren Weibo; Xu Zhu; Chen Libo; Guo Huiqin; Wang Mi; Zhao Liang

2008-01-01

To understand the cytological effects of space flight on alfalfa seeds, dry seeds of three lines (Line 1, Line 2 and Line 4) were selected and loaded onto 'Shijian No.8' satellite for space flight. After returning to the ground, root tips of alfalfa were clipped and chromosome aberrations were observed by microscope. Data showed that space flight had two types of effect on cell mitotic: one was positive (Line 2, Line 4) and the other was negative (Line 1). Such chromosome aberrations were observed as micronucleus, chromosome bridge, fragments, lagging and so on. The frequency of aberration varied with the different materials. Conclusion was that space flight had significant effect on root tip cells, which mainly showed as the chromosome aberrations. (authors)

Flight Test of an Intelligent Flight-Control System

Science.gov (United States)

Davidson, Ron; Bosworth, John T.; Jacobson, Steven R.; Thomson, Michael Pl; Jorgensen, Charles C.

2003-01-01

inputs with the outputs provided to instrumentation only. The IFCS was not used to control the airplane. In another stage of the flight test, the Phase I pre-trained neural network was integrated into a Phase III version of the flight control system. The Phase I pretrained neural network provided realtime stability and control derivatives to a Phase III controller that was based on a stochastic optimal feedforward and feedback technique (SOFFT). This combined Phase I/III system was operated together with the research flight-control system (RFCS) of the F-15 ACTIVE during the flight test. The RFCS enables the pilot to switch quickly from the experimental- research flight mode back to the safe conventional mode. These initial IFCS ACP flight tests were completed in April 1999. The Phase I/III flight test milestone was to demonstrate, across a range of subsonic and supersonic flight conditions, that the pre-trained neural network could be used to supply real-time aerodynamic stability and control derivatives to the closed-loop optimal SOFFT flight controller. Additional objectives attained in the flight test included (1) flight qualification of a neural-network-based control system; (2) the use of a combined neural-network/closed-loop optimal flight-control system to obtain level-one handling qualities; and (3) demonstration, through variation of control gains, that different handling qualities can be achieved by setting new target parameters. In addition, data for the Phase-II (on-line-learning) neural network were collected, during the use of stacked-frequency- sweep excitation, for post-flight analysis. Initial analysis of these data showed the potential for future flight tests that will incorporate the real-time identification and on-line learning aspects of the IFCS.

ALARM, a life saving training program for inpatient mental health care staff. Tallinn, Estland (27-30 augustus 2014) : Oral presentation European Symposium on Suicide and Suicidal Behaviour

NARCIS (Netherlands)

Nienke Kool

2014-01-01

Oral presentation European Symposium on Suicide and Suicidal Behaviour. Titel: ALARM, a life saving training program for inpatient mental health care staff. Tallinn, Estland (27-30 augustus 2014) Introduction Despite precautions, suicide does happen. Sometimes patients are found while attempting

Kohtumispaigad: Tallinna kohvikute interjööre = Meeting Places : Interiors of Tallinn Cafes / Kai Lobjakas ; tõlk. Laila Põdra

Index Scriptorium Estoniae

Lobjakas, Kai, 1975-

2003-01-01

Tallinna kohvikutest aastail 1930-2003. Vaadeldakse kohvikuid Corso/Harju, Feischner/Tallinn, Palace, Kultas/Moskva, Energia, Narva, Pärl, Pegasus, Tuluke, Szolnok, Tuljak, Vigri, Toome, Corrida, Võitlev Sõna, Robert's Coffee, Rossini, Popular. Sisekujundajad: R. Natus, V. Tomassov, K. Herman, B. Linde, J. Siirak, V. Asi, V. Tamm, L. Pärtelpoeg, N. Kultas, P. Aren, H. Karro, G. Nahkur, L. Tarvas, M. Grünberg, A. Murdmaa, M. Tammik, G. Sarv, A. Maasik, A. Nurk, R. Treu, M. Sulengo, R. Tiitus. 22 vaadet, kaart

[Nordosteuropa als Geschichtsregion. Beiträge des III. Internationalen Symposiums zur deutschen Kultur und Geschichte im europäischen Nordosten vom 20.-22. September 2001 in Tallinn

Index Scriptorium Estoniae

Lawaty, Andreas

2011-01-01

Arvustus : Nordosteuropa als Geschichtsregion. Beiträge des III. Internationalen Symposiums zur deutschen Kultur und Geschichte im europäischen Nordosten vom 20.-22. September 2001 in Tallinn. Lübeck : Verlag Schmidt-Römhild 2006. (Veröffentlihungen der Aue-Stiftung. 17)

Eesti Gaas. Inspection of Kohtal-Jaerve - Tallinn pipeline. Final report

Energy Technology Data Exchange (ETDEWEB)

NONE

1996-11-01

The project `Inspection of Pipelines in Estonia` was funded by Danish government and was carried out in collaboration between DONG, Balslev and FORCE. By agreement between Eesti Gaas and DONG, the pipeline system between Kohtla-Jaerve and Tallinn was selected for inspection. This pipeline system has a total length of 176.9 km. The objective of the project has been, based on detailed inspection of relative short lengths of pipe, to determine the integrity of the pipeline and to give advice concerning the continued use as a high pressure transmission pipeline. The objectives have been met as set out by the project Proposal with the investigation and this report as follows: Based on a document review together with the measurements and observations in the field and in the laboratory, the condition of approximately 5 km of the pipeline has been evaluated; Recommendations are given in this report with the aim of extending the life of the pipeline. A further objective has been to provide know-how transfer in order to permit Eesti Gaas to run similar inspections on other parts of their transmission system. (EG)

Health impact assessment of particulate pollution in Tallinn using fine spatial resolution and modeling techniques

Directory of Open Access Journals (Sweden)

Kimmel Veljo

2009-03-01

Full Text Available Abstract Background Health impact assessments (HIA use information on exposure, baseline mortality/morbidity and exposure-response functions from epidemiological studies in order to quantify the health impacts of existing situations and/or alternative scenarios. The aim of this study was to improve HIA methods for air pollution studies in situations where exposures can be estimated using GIS with high spatial resolution and dispersion modeling approaches. Methods Tallinn was divided into 84 sections according to neighborhoods, with a total population of approx. 390 000 persons. Actual baseline rates for total mortality and hospitalization with cardiovascular and respiratory diagnosis were identified. The exposure to fine particles (PM2.5 from local emissions was defined as the modeled annual levels. The model validation and morbidity assessment were based on 2006 PM10 or PM2.5 levels at 3 monitoring stations. The exposure-response coefficients used were for total mortality 6.2% (95% CI 1.6–11% per 10 μg/m3 increase of annual mean PM2.5 concentration and for the assessment of respiratory and cardiovascular hospitalizations 1.14% (95% CI 0.62–1.67% and 0.73% (95% CI 0.47–0.93% per 10 μg/m3 increase of PM10. The direct costs related to morbidity were calculated according to hospital treatment expenses in 2005 and the cost of premature deaths using the concept of Value of Life Year (VOLY. Results The annual population-weighted-modeled exposure to locally emitted PM2.5 in Tallinn was 11.6 μg/m3. Our analysis showed that it corresponds to 296 (95% CI 76528 premature deaths resulting in 3859 (95% CI 10236636 Years of Life Lost (YLL per year. The average decrease in life-expectancy at birth per resident of Tallinn was estimated to be 0.64 (95% CI 0.17–1.10 years. While in the polluted city centre this may reach 1.17 years, in the least polluted neighborhoods it remains between 0.1 and 0.3 years. When dividing the YLL by the number of

[Kreem, Juhan. Sketches of a Clerk. Pen-and-ink Drawings in the Margins of the Medieval Accoung Books of Reval (Tallinn)] / Anu Mänd

Index Scriptorium Estoniae

Mänd, Anu, 1968-

2008-01-01

Arvustus: Kreem, Juhan. Sketches of a Clerk. Pen-and-ink Drawings in the Margins of the Medieval Accoung Books of Reval (Tallinn). (Krems, 2006). Juhan Kreemi raamat käsitleb Tallinna rae keskaegsetes arveraamatutes leiduvaid sulejoonistusi. Autor on välja selgitanud nende, esmapilgul juhuslikena näivate joonistuste otstarbe ning püüdnud nende kaudu avada tolleaegsete linnaametnike mõttemalle

[Nordosteuropa als Geschichtsregion : Beiträge des III. Internationalen Symposiums zur Deutschen Kultur und Geschichte im Europäischen Nordosten vom 20. - 22. September 2001 in Tallinn (Estland)] / Janet Laidla

Index Scriptorium Estoniae

Laidla, Janet, 1982-

2008-01-01

Arvustus: Nordosteuropa als Geschichtsregion : Beiträge des III. Internationalen Symposiums zur Deutschen Kultur und Geschichte im Europäischen Nordosten vom 20. - 22. September 2001 in Tallinn (Estland). (Helsinki : Aue-Stiftung ; Lübeck : Scmidt-Römhild, 2006)

IRVE-II Post-Flight Trajectory Reconstruction

Science.gov (United States)

O'Keefe, Stephen A.; Bose, David M.

2010-01-01

NASA s Inflatable Re-entry Vehicle Experiment (IRVE) II successfully demonstrated an inflatable aerodynamic decelerator after being launched aboard a sounding rocket from Wallops Flight Facility (WFF). Preliminary day of flight data compared well with pre-flight Monte Carlo analysis, and a more complete trajectory reconstruction performed with an Extended Kalman Filter (EKF) approach followed. The reconstructed trajectory and comparisons to an attitude solution provided by NASA Sounding Rocket Operations Contract (NSROC) personnel at WFF are presented. Additional comparisons are made between the reconstructed trajectory and pre and post-flight Monte Carlo trajectory predictions. Alternative observations of the trajectory are summarized which leverage flight accelerometer measurements, the pre-flight aerodynamic database, and on-board flight video. Finally, analysis of the payload separation and aeroshell deployment events are presented. The flight trajectory is reconstructed to fidelity sufficient to assess overall project objectives related to flight dynamics and overall, IRVE-II flight dynamics are in line with expectations

Lahesõjas viik / Ain Hinsberg

Index Scriptorium Estoniae

Hinsberg, Ain

2001-01-01

Helsingi ja Tallinna vahel liikuvate laevafirmade konkurents: Silja Line, Nordic Jet Line, Tallink ja Linda Line. Tabelid: reisijad laevaliinil Helsingi-Tallinn 1998-2001; Helsingi-Tallinna liinil kiirlaevade turuosad 1999-2000

Off-line correction for excessive constant-fraction-discriminator walk in neutron time-of-flight experiments

International Nuclear Information System (INIS)

Heilbronn, Lawrence; Iwata, Yoshiyuki; Iwase, H.

2003-01-01

A method for reducing excessive constant-fraction-discriminator walk that utilizes experimental data in the off-line analysis stage is introduced. Excessive walk is defined here as any walk that leads to an overall timing resolution that is much greater than the intrinsic timing resolution of the detection system. The method is able to reduce the contribution to the overall timing resolution from the walk that is equal to or less than the intrinsic timing resolution of the detectors. Although the method is explained in the context of a neutron time-of-flight experiment, it is applicable to any data set that satisfies two conditions. (1) A measure of the signal amplitude for each event must be recorded on an event-by-event basis; and (2) There must be a distinguishable class of events present where the timing information is known a priori

Off-line correction for excessive constant-fraction-discriminator walk in neutron time-of-flight experiments

International Nuclear Information System (INIS)

Heilbronn, L.; Iwata, Y.; Iwase, H.

2004-01-01

A method for reducing excessive constant-fraction-discriminator walk that utilizes experimental data in the off-line analysis stage is introduced. Excessive walk is defined here as any walk that leads to an overall timing resolution that is much greater than the intrinsic timing resolution of the detection system. The method is able to reduce the contribution to the overall timing resolution from the walk to a value that is equal to or less than the intrinsic timing resolution of the detectors. Although the method is explained in the context of a neutron time-of-flight experiment, it is applicable to any data set that satisfies two conditions: (1) a measure of the signal amplitude for each event must be recorded on an event-by-event basis; and (2) there must be a distinguishable class of events present where the timing information is known a priori

Flight Test Evaluation of an Unmanned Aircraft System Traffic Management (UTM) Concept for Multiple Beyond-Visual-Line-of-Sight (BVLOS) Operations

Science.gov (United States)

Johnson, Marcus; Jung, Jaewoo; Rios, Joseph; Mercer, Joey; Homola, Jeffrey; Prevot, Thomas; Mulfinger, Daniel; Kopardekar, Parimal

2017-01-01

Many applications of small Unmanned Aircraft System (UAS) have been envisioned. These include surveillance of key assets such as pipelines, rail, or electric wires, deliveries, search and rescue, traffic monitoring, videography, and precision agriculture. These operations are likely to occur in the same airspace in the presence of many static and dynamic constraints such as airports, and high wind areas. Therefore, operations of small UAS need to be managed to ensure safety and operation efficiency is maintained. NASA has advanced a concept for UAS Traffic Management (UTM) and has initiated a research effort to refine that concept and develop operational and system requirements. A UTM research platform is in development and flight test activities to evaluate core functions and key assumptions focusing exclusively on UAS operations in different environments are underway. This seminar will present lessons learned from a recent flight test focused on enabling operations of multiple UAS in lower-risk environments within and beyond visual line of sight (BVLOS).

Metabolomics Characterization of U.S. and Japanese F-15 and C-130 Flight Line Crews Exposed to Jet Fuel Volatile Organic Compounds and Aerosols

Science.gov (United States)

2014-09-30

been recognized as the single largest source of chemical exposure for U.S. and NATO military personnel (Carlton and Smith, 2000) where inhalation and...flight line, 2) exposure to spills, 3) inhalation exposure (primarily exhaust), and 4) total measured VOCs. The total VOC value was calculated by...chemical and primary metals industries, biomass burning, gasoline and oil combustion, tobacco smoking, the use of mothballs, fumigants and deodorizers

Flight Control of the High Altitude Wind Power System

NARCIS (Netherlands)

Podgaets, A.R.; Ockels, W.J.

2007-01-01

Closed loop Laddermill flight control problem is considered in this paper. Laddermill is a high altitude kites system for energy production. The kites have been simulated as rigid bodies and the cable as a thin elastic line. Euler angles and cable speed are controls. Flight control is written as a

Efficacy of convenience sampling through the internet versus respondent driven sampling among males who have sex with males in Tallinn and Harju County, Estonia: challenges reaching a hidden population.

Science.gov (United States)

Johnston, Lisa Grazina; Trummal, Aire; Lohmus, Liilia; Ravalepik, Ardi

2009-09-01

This paper examines challenges obtaining representative samples of males who have sex with males (MSM) in Estonia and provides descriptive HIV behavioral data gathered from four cross-sectional surveys; three using the internet, and one using respondent driven sampling (RDS) to recruit MSM in Tallinn and Harju County. Estonian MSM were sampled between March and May in 2004 (n=193), August and November in 2005 (n=146) and September and December in 2007 (n=238) using internet websites. MSM in Tallinn and Harju County were sampled between April and June in 2007 (n=59) using RDS. Recruitment of MSM using RDS did not acquire the calculated sample size. The RDS study reached a less diverse group of MSM than did the internet studies which recruited a larger proportion of MSM who were older, bisexual, having female sexual partners during the last six months, and unlikely to have been tested for HIV. The findings and observations presented in this paper could inform researchers in Estonia, and the region, about the efficacy of and socio-cultural challenges to sampling MSM to collect HIV biological and/or behavioral data.

An on-line monitoring system for navigation equipment

Science.gov (United States)

Wang, Bo; Yang, Ping; Liu, Jing; Yang, Zhengbo; Liang, Fei

2017-10-01

Civil air navigation equipment is the most important infrastructure of Civil Aviation, which is closely related to flight safety. In addition to regular flight inspection, navigation equipment's patrol measuring, maintenance measuring, running measuring under special weather conditions are the important means of ensuring aviation flight safety. According to the safety maintenance requirements of Civil Aviation Air Traffic Control navigation equipment, this paper developed one on-line monitoring system with independent intellectual property rights for navigation equipment, the system breakthroughs the key technologies of measuring navigation equipment on-line including Instrument Landing System (ILS) and VHF Omni-directional Range (VOR), which also meets the requirements of navigation equipment ground measurement set by the ICAO DOC 8071, it provides technical means of the ground on-line measurement for navigation equipment, improves the safety of navigation equipment operation, and reduces the impact of measuring navigation equipment on airport operation.

Time-of-flight experiments using a pseudo-statistical chopper

International Nuclear Information System (INIS)

Aizawa, Otohiko; Kanda, Keiji

1975-01-01

A ''pseudo-statistical'' chopper was manufactured and used for the experiments on neutron transmission and scattering. The characteristics of the chopper and the experimental results are discussed in comparison with those in the time-of-flight technique using a conventional chopper. Which of the two methods is superior depends on the form of the time-of-flight distribution to be measured. Pseudo-statistical pulsing may be especially advantageous for scattering experiments with single or a few-line time-of-flight spectrum. (auth.)

Simbol-X Formation Flight and Image Reconstruction

Science.gov (United States)

Civitani, M.; Djalal, S.; Le Duigou, J. M.; La Marle, O.; Chipaux, R.

2009-05-01

Simbol-X is the first operational mission relying on two satellites flying in formation. The dynamics of the telescope, due to the formation flight concept, raises a variety of problematic, like image reconstruction, that can be better evaluated via a simulation tools. We present here the first results obtained with Simulos, simulation tool aimed to study the relative spacecrafts navigation and the weight of the different parameters in image reconstruction and telescope performance evaluation. The simulation relies on attitude and formation flight sensors models, formation flight dynamics and control, mirror model and focal plane model, while the image reconstruction is based on the Line of Sight (LOS) concept.

Fatal traffic injuries among children and adolescents in three cities (capital Budapest, Vilnius, and Tallinn).

Science.gov (United States)

Töro, Klára; Szilvia, Fehér; György, Dunay; Pauliukevicius, Alvydas; Caplinskiene, Marija; Raudys, Romas; Lepik, Delia; Tuusov, Jana; Vali, Marika

2011-05-01

Motor vehicle accidental injuries are a frequent cause of death among young children and adolescents. The goal of this study was to compare patterns of injury between three capitals (Budapest, Vilnius, and Tallinn). Information on 190 fatal traffic accidents (69 pedestrians, 14 bicyclists, and 107 motor vehicle occupants) between 2002 and 2006 was collected from databases of medico-legal autopsies. The role of victims in accidents, the location of injuries, cause of death, survival period, and blood alcohol levels were evaluated. One-hundred and forty-one (74%) victims had a passive role in traffic as pedestrians, passengers in cars, or public transport. In victims who died at the scene, the rate of head injury was higher than in cases who received medical treatment (odds ratio = 2.58, CI = 1.2-5.55, p = 0.0127). These results underline the importance of postmortem studies to examine the pathomechanism of fatal traffic accidental injuries and to provide information for the prevention of road traffic accidents against children and adolescents. © 2011 American Academy of Forensic Sciences.

Respiratory Evolution Facilitated the Origin of Pterosaur Flight and Aerial Gigantism

OpenAIRE

Claessens, Leon P. A. M.; O'Connor, Patrick M.; Unwin, David M.

2009-01-01

Pterosaurs, enigmatic extinct Mesozoic reptiles, were the first vertebrates to achieve true flapping flight. Various lines of evidence provide strong support for highly efficient wing design, control, and flight capabilities. However, little is known of the pulmonary system that powered flight in pterosaurs. We investigated the structure and function of the pterosaurian breathing apparatus through a broad scale comparative study of respiratory structure and function in living and extinct arch...

Quantifying Pilot Contribution to Flight Safety During an In-Flight Airspeed Failure

Science.gov (United States)

Etherington, Timothy J.; Kramer, Lynda J.; Bailey, Randall E.; Kennedey, Kellie D.

2017-01-01

Accident statistics cite the flight crew as a causal factor in over 60% of large transport fatal accidents. Yet a well-trained and well-qualified crew is acknowledged as the critical center point of aircraft systems safety and an integral component of the entire commercial aviation system. A human-in-the-loop test was conducted using a Level D certified Boeing 737-800 simulator to evaluate the pilot's contribution to safety-of-flight during routine air carrier flight operations and in response to system failures. To quantify the human's contribution, crew complement was used as an independent variable in a between-subjects design. This paper details the crew's actions and responses while dealing with an in-flight airspeed failure. Accident statistics often cite flight crew error (Baker, 2001) as the primary contributor in accidents and incidents in transport category aircraft. However, the Air Line Pilots Association (2011) suggests "a well-trained and well-qualified pilot is acknowledged as the critical center point of the aircraft systems safety and an integral safety component of the entire commercial aviation system." This is generally acknowledged but cannot be verified because little or no quantitative data exists on how or how many accidents/incidents are averted by crew actions. Anecdotal evidence suggest crews handle failures on a daily basis and Aviation Safety Action Program data generally supports this assertion, even if the data is not released to the public. However without hard evidence, the contribution and means by which pilots achieve safety of flight is difficult to define. Thus, ways to improve the human ability to contribute or overcome deficiencies are ill-defined.

Assessing UAS Flight Testing and It's Importance for Beyond-Line-of-Sight UAS Control in Cooperation with Partnering Organizations

Science.gov (United States)

de Jong, Daphne

2015-01-01

From the 1st of June until the 21st of August, the internship has been conducted at NASA Ames Research Center as part of the Master of Space Studies at the International Space University. The main activities consisted of doing research on UAV flight-­-testing and the assessing of safety with respect to Beyond-­-Line-­-Of-­-Sight operations. Further activities consisted of accommodating international partners and potential partners at the NASA Ames site, in order to identify mutual interest and future collaboration. Besides those activities, the report describes the planning process of the ISU Space Coast Trip to 10 different space related companies on the west-­-coast of California. Key words: UAS, UAV, BLOS, Ames, ISU Trip

THE INFLUENCE OF SOCIAL STATUS AND ETHNICITY ON DIET IN MEDIAEVAL TALLINN AS SEEN THROUGH STABLE ISOTOPE ANALYSIS

DEFF Research Database (Denmark)

Lightfoot, Emma; Naum, Magdalena; Kadakas, Villu

2016-01-01

, for comparative purposes. The individuals were investigated using carbon, nitrogen and oxygen stable isotope analysis. The results indicate that while all analysed individuals consumed diets based on C3 plants and animals consuming C3 plants, some individuals also consumed small amounts of C4 plants (likely......Food encodes social and cultural values and has an important role to play in defining identities. In mixed populations, diet can be used to distinguish between ‘us’ and ‘them’. This study investigates the extent to which the inhabitants of mediaeval Tallinn, an important trading centre, used food...... millet) or seafood. C 4 plants were consumed by the urban residents buried at the Church of the Holy Spirit and one or two individuals from Sulevimägi. It is thought that millet was an imported food consumed by the middle class. Marine foods were consumed by the individuals at St Catherine’s Church...

NASA/RAE cooperation on a knowlede based flight status monitor

Science.gov (United States)

Butler, G. F.; Duke, E. L.

1989-01-01

As part of a US/UK cooperative aeronautical research pragram, a joint activity between the Dryden Flight Research Facility of the NASA Ames Research Center (Ames-Dryden) and the Royal Aerospace Establishment (RAE) on Knowledge Based Systems was established. Under the agreement, a Flight Status Monitor Knowledge base developed at Ames-Dryden was implemented using the real-time IKBS toolkit, MUSE, which was developed in the UK under RAE sponsorship. The Flight Status Monitor is designed to provide on-line aid to the flight test engineer in the interpretation of system health and status by storing expert knowledge of system behavior in an easily accessible form. The background to the cooperation is described and the details of the Flight Status Monitor, the MUSE implementation are presented.

ALICE Time of Flight Module

CERN Multimedia

The Time-Of-Flight system of ALICE consists of 90 such modules, each containing 15 or 19 Multigap Resistive Plate Chamber (MRPC) strips. This detector is used for identification of charged particles. It measures with high precision (50 ps) the time of flight of charged particles and therefore their velocity. The curvature of the particle trajectory inside the magnetic field gives the momentum, thus the particle mass is calculated and the particle is identified The MRPC is a stack of resistive glass plates, separated from each other by nylon fishing line. The mass production of the chambers (~1600, covering a surface of 150 m2) was done at INFN Bologna, while the first prototypes were bult at CERN.

Method for Pedestrian Crossing Risk Assessment and Safety Level Determination: the Case Study of Tallinn

Energy Technology Data Exchange (ETDEWEB)

Pashkevich, M.; Krasilnikova, A.; Antov, D.

2016-07-01

Pedestrians are a part of vulnerable road users which safety requires a special attention. Official statistics in Estonia from the last decade returns the following numbers: around 30 % of all road traffic accidents in the country were accidents with pedestrians, 32 % of all traffic fatalities were finished with pedestrian death. Pedestrian crossing has the biggest risk level between all kinds of pedestrian facilities, because it includes a direct conflict point between vehicle and pedestrian traffics. The article presents a method to assess risk of pedestrian crossing users and to determine safety level of this road infrastructure element. This approach is based on observation and collection of infrastructural as well as traffic data, which includes: (1) information about each pedestrian crossing facility, its location and state, (2) data about accidents with pedestrians and their features, (3) data from road traffic measurements. The main advantages of the described method are universality and comprehensiveness. The case study was done in Kristiine district of the city Tallinn, which was chosen as the most typical average district of Estonian capital. Results of this study are also presented in the article. (Author)

TRENDS IN URBAN STORM WATER QUALITY IN TALLINN AND INFLUENCES FROM STORMFLOW AND BASEFLOW

Directory of Open Access Journals (Sweden)

Bharat Maharjan

2016-04-01

Full Text Available Temporal trends provide a good interpretation of change in stormwater quality over time. This study aimed to analyse trends and influences due to stormflow and baseflow. Grab samples of 18-19 years from 1995 to 2014 recorded at outlets of 7 Tallinn watersheds were analysed for monotonic trend through seasonal Mann Kendall test for long-term, short-term, baseflow and stormflow. Statistically significant downward trends (P-value (p 0.05 and < 0.2 for 3 – SS, 1 – BOD, 1 – TN and 1 – TP were identified. Statistically significant long-term upward trends of pH were revealed in 5 basins, which reduced to 2 with 5 less significant upward trends over the 10 year period, indicating improvements in pH reduction. Härjapea has the highest pH without trend but it includes an upward trend of TN at p = 0.051. The highly possible causes for downward trends are street sweeping, sewer network improvement, decline in sub-urban agricultural areas, etc. The upward trend results of pH are related to increased alkalinisation due to acidic rain, weathering of carbonate rocks, sewage discharge and alkaline road dust. In most of the basins, stormflow has more influence on trends than baseflow.

Analytical properties of time-of-flight PET data

Energy Technology Data Exchange (ETDEWEB)

Cho, Sanghee; Ahn, Sangtae; Quanzheng, Li; Leahy, Richard M [Signal and Image Processing Institute, University of Southern California, Los Angeles, CA 90089 (United States)], E-mail: leahy@sipi.usc.edu

2008-06-07

We investigate the analytical properties of time-of-flight (TOF) positron emission tomography (PET) sinograms, where the data are modeled as line integrals weighted by a spatially invariant TOF kernel. First, we investigate the Fourier transform properties of 2D TOF data and extend the 'bow-tie' property of the 2D Radon transform to the time-of-flight case. Second, we describe a new exact Fourier rebinning method, TOF-FOREX, based on the Fourier transform in the time-of-flight variable. We then combine TOF-FOREX rebinning with a direct extension of the projection slice theorem to TOF data, to perform fast 3D TOF PET image reconstruction. Finally, we illustrate these properties using simulated data.

Analytical properties of time-of-flight PET data

Science.gov (United States)

Cho, Sanghee; Ahn, Sangtae; Li, Quanzheng; Leahy, Richard M.

2008-06-01

We investigate the analytical properties of time-of-flight (TOF) positron emission tomography (PET) sinograms, where the data are modeled as line integrals weighted by a spatially invariant TOF kernel. First, we investigate the Fourier transform properties of 2D TOF data and extend the 'bow-tie' property of the 2D Radon transform to the time-of-flight case. Second, we describe a new exact Fourier rebinning method, TOF-FOREX, based on the Fourier transform in the time-of-flight variable. We then combine TOF-FOREX rebinning with a direct extension of the projection slice theorem to TOF data, to perform fast 3D TOF PET image reconstruction. Finally, we illustrate these properties using simulated data.

Analytical properties of time-of-flight PET data

International Nuclear Information System (INIS)

Cho, Sanghee; Ahn, Sangtae; Li Quanzheng; Leahy, Richard M

2008-01-01

We investigate the analytical properties of time-of-flight (TOF) positron emission tomography (PET) sinograms, where the data are modeled as line integrals weighted by a spatially invariant TOF kernel. First, we investigate the Fourier transform properties of 2D TOF data and extend the 'bow-tie' property of the 2D Radon transform to the time-of-flight case. Second, we describe a new exact Fourier rebinning method, TOF-FOREX, based on the Fourier transform in the time-of-flight variable. We then combine TOF-FOREX rebinning with a direct extension of the projection slice theorem to TOF data, to perform fast 3D TOF PET image reconstruction. Finally, we illustrate these properties using simulated data

Analytical properties of time-of-flight PET data

Energy Technology Data Exchange (ETDEWEB)

Cho, Sanghee; Ahn, Sangtae; Li Quanzheng; Leahy, Richard M [Signal and Image Processing Institute, University of Southern California, Los Angeles, CA 90089 (United States)], E-mail: leahy@sipi.usc.edu

2008-06-07

We investigate the analytical properties of time-of-flight (TOF) positron emission tomography (PET) sinograms, where the data are modeled as line integrals weighted by a spatially invariant TOF kernel. First, we investigate the Fourier transform properties of 2D TOF data and extend the 'bow-tie' property of the 2D Radon transform to the time-of-flight case. Second, we describe a new exact Fourier rebinning method, TOF-FOREX, based on the Fourier transform in the time-of-flight variable. We then combine TOF-FOREX rebinning with a direct extension of the projection slice theorem to TOF data, to perform fast 3D TOF PET image reconstruction. Finally, we illustrate these properties using simulated data.

Annual view (1999) - aeronautic relation/space relation. Aeronautic relation - flight preparation; Nenkan tenbo (1999) koku kankei uchu kankei. Unko seibi kanren

Energy Technology Data Exchange (ETDEWEB)

NONE

2000-03-05

The year of 1999 to airline companies was exactly a year when they had to tackle the Y2K issue all the time with no introduction of new model planes. For the purpose of much appealing for aeronautical safety, the government and private companies jointly made a demonstration flight simulating the shift to a new year in September. The persons concerned in the Civil Aviation Bureau, the Ministry of Transport, mass communication, and airline companies were on the flight. The demonstration flight was finished with no big troubles. The standard weight of passengers, etc. which is used for weight/gravity center position management of airliners was to be newly set. Following the domestic line in 1998, the standard weight of the international line was set in 1999. As a new flight system, RVSM flight is planned to be started in the Pacific air area in February 2000. In the RVSM flight, airplane is flown by shortening vertical control intervals from 2000ft to 1000ft at the altitude between 29,000ft and 41,000ft. In 1999, domestic airline companies decided on no smoking at all the seats in both the domestic line and international line. (NEDO)

Plaadid : Pop& rock. Retro. Jazz. Klassika

Index Scriptorium Estoniae

2002-01-01

Uutest plaatidest. Sisqo "Return Of Dragon", Alice Cooper "Dragontown", Kim Wilde "The Very Best Of", David Sanches "Travesia", Peter White "Glow". Eesti plaadid : Vennaskond "News From Nowhere", Erinevad esitajad "Tallinn. Psühhedeelne linn", Ivo Linna "Enne ja pärast päeva", Arne Oit & Margus Kappel "Unustuste jõel", Anu Tali "Swan Flight"

Rootsi rangus kimbutab Tallinkit lisanõuetega / Lauri Linnamäe

Index Scriptorium Estoniae

Linnamäe, Lauri

2007-01-01

Rootsi mereinspektorid leidsid puudusi veekindlate uste elektrisüsteemides Tallinki laevadel Regina Baltica ja Vana Tallinn ning Viking Line'i Mariellal, kirjutab Rootsi meedia. Vt. samas: Galaxy vahetab lippu

On the typography of flight-deck documentation

Science.gov (United States)

Degani, Asaf

1992-01-01

Many types of paper documentation are employed on the flight-deck. They range from a simple checklist card to a bulky Aircraft Flight Manual (AFM). Some of these documentations have typographical and graphical deficiencies; yet, many cockpit tasks such as conducting checklists, way-point entry, limitations and performance calculations, and many more, require the use of these documents. Moreover, during emergency and abnormal situations, the flight crews' effectiveness in combating the situation is highly dependent on such documentation; accessing and reading procedures has a significant impact on flight safety. Although flight-deck documentation are an important (and sometimes critical) form of display in the modern cockpit, there is a dearth of information on how to effectively design these displays. The object of this report is to provide a summary of the available literature regarding the design and typographical aspects of printed matter. The report attempts 'to bridge' the gap between basic research about typography, and the kind of information needed by designers of flight-deck documentation. The report focuses on typographical factors such as type-faces, character height, use of lower- and upper-case characters, line length, and spacing. Some graphical aspects such as layout, color coding, fonts, and character contrast are also discussed. In addition, several aspects of cockpit reading conditions such as glare, angular alignment, and paper quality are addressed. Finally, a list of recommendations for the graphical design of flight-deck documentation is provided.

Acoustic Wave Propagation in Pressure Sense Lines

Science.gov (United States)

Vitarius, Patrick; Gregory, Don A.; Wiley, John; Korman, Valentin

2003-01-01

Sense lines are used in pressure measurements to passively transmit information from hostile environments to areas where transducers can be used. The transfer function of a sense line can be used to obtain information about the measured environment from the protected sensor. Several properties of this transfer function are examined, including frequency dependence, Helmholtz resonance, and time of flight delay.

Radiation exposure on flights; Strahlenexposition beim Fliegen. Ein Fall fuer den Strahlenschutz

Energy Technology Data Exchange (ETDEWEB)

Blettner, Maria [Mainz Univ. (Germany). Inst. fuer Medizinische Biometrie, Epidemiologie und Informatik (IMBEI); Boehm, Theresia; Eberbach, Frieder [Vereinigung Cockpit e.V. Main Airport Center (MAC), Frankfurt (Germany). AG Strahlenschutz; Bottollier-Depois, Jean-Francois [Institut de Radioprotection et de Surete Nucleaire (IRSN), Fontenay-aux-Roses (France); Clairand, Isabelle; Huet, Christelle [Institut de Radioprotection et de Surete Nucleaire (IRSN), Fontenay-aux-Roses (France). Ionizing Radiation Dosimetry Lab.; Frasch, Gerhard [Bundesamt fuer Strahlenschutz, Oberschleissheim/Neuherberg (Germany). Beruflicher Strahlenschutz und Strahlenschutzregister; Hammer, Ga el P. [Laboratoire National de Sante E.P., Dudelange (Luxembourg). Registre Morphologique des Tumeurs; Mares, Vladimir; Ruehm, Werner [Helmholtz Zentrum Muenchen Deutsches Forschungszentrum fuer Gesundheit und Umwelt GmbH, Neuherberg (Germany); Voelkle, Hansruedi [Fribourg Univ. (Switzerland). Physikdept.

2014-09-01

Extend and effects of radiation doses occuring during flights are treated under various aspects. Part of them are, in the first line, radiation exposure of the flying staff and the results of epidemiologic studies regarding the health consequences, as well as aspects of practical radiation protection for the flying staff. Computer programs for dose calculation on flights round off the theme. (orig.)

X-36 in Flight over Mojave Desert during 5th Flight

Science.gov (United States)

1997-01-01

The unusual lines of the X-36 Tailless Fighter Agility Research Aircraft contrast sharply with the desert floor as the remotely-piloted aircraft flies over the Mojave Desert on a June 1997 research flight. The NASA/Boeing X-36 Tailless Fighter Agility Research Aircraft program successfully demonstrated the tailless fighter design using advanced technologies to improve the maneuverability and survivability of possible future fighter aircraft. The program met or exceeded all project goals. For 31 flights during 1997 at the Dryden Flight Research Center, Edwards, California, the project team examined the aircraft's agility at low speed / high angles of attack and at high speed / low angles of attack. The aircraft's speed envelope reached up to 206 knots (234 mph). This aircraft was very stable and maneuverable. It handled very well. The X-36 vehicle was designed to fly without the traditional tail surfaces common on most aircraft. Instead, a canard forward of the wing was used as well as split ailerons and an advanced thrust-vectoring nozzle for directional control. The X-36 was unstable in both pitch and yaw axes, so an advanced, single-channel digital fly-by-wire control system (developed with some commercially available components) was put in place to stabilize the aircraft. Using a video camera mounted in the nose of the aircraft and an onboard microphone, the X-36 was remotely controlled by a pilot in a ground station virtual cockpit. A standard fighter-type head-up display (HUD) and a moving-map representation of the vehicle's position within the range in which it flew provided excellent situational awareness for the pilot. This pilot-in-the-loop approach eliminated the need for expensive and complex autonomous flight control systems and the risks associated with their inability to deal with unknown or unforeseen phenomena in flight. Fully fueled the X-36 prototype weighed approximately 1,250 pounds. It was 19 feet long and three feet high with a wingspan of

Respiratory evolution facilitated the origin of pterosaur flight and aerial gigantism.

Directory of Open Access Journals (Sweden)

Leon P A M Claessens

Full Text Available Pterosaurs, enigmatic extinct Mesozoic reptiles, were the first vertebrates to achieve true flapping flight. Various lines of evidence provide strong support for highly efficient wing design, control, and flight capabilities. However, little is known of the pulmonary system that powered flight in pterosaurs. We investigated the structure and function of the pterosaurian breathing apparatus through a broad scale comparative study of respiratory structure and function in living and extinct archosaurs, using computer-assisted tomographic (CT scanning of pterosaur and bird skeletal remains, cineradiographic (X-ray film studies of the skeletal breathing pump in extant birds and alligators, and study of skeletal structure in historic fossil specimens. In this report we present various lines of skeletal evidence that indicate that pterosaurs had a highly effective flow-through respiratory system, capable of sustaining powered flight, predating the appearance of an analogous breathing system in birds by approximately seventy million years. Convergent evolution of gigantism in several Cretaceous pterosaur lineages was made possible through body density reduction by expansion of the pulmonary air sac system throughout the trunk and the distal limb girdle skeleton, highlighting the importance of respiratory adaptations in pterosaur evolution, and the dramatic effect of the release of physical constraints on morphological diversification and evolutionary radiation.

Respiratory evolution facilitated the origin of pterosaur flight and aerial gigantism.

Science.gov (United States)

Claessens, Leon P A M; O'Connor, Patrick M; Unwin, David M

2009-01-01

Pterosaurs, enigmatic extinct Mesozoic reptiles, were the first vertebrates to achieve true flapping flight. Various lines of evidence provide strong support for highly efficient wing design, control, and flight capabilities. However, little is known of the pulmonary system that powered flight in pterosaurs. We investigated the structure and function of the pterosaurian breathing apparatus through a broad scale comparative study of respiratory structure and function in living and extinct archosaurs, using computer-assisted tomographic (CT) scanning of pterosaur and bird skeletal remains, cineradiographic (X-ray film) studies of the skeletal breathing pump in extant birds and alligators, and study of skeletal structure in historic fossil specimens. In this report we present various lines of skeletal evidence that indicate that pterosaurs had a highly effective flow-through respiratory system, capable of sustaining powered flight, predating the appearance of an analogous breathing system in birds by approximately seventy million years. Convergent evolution of gigantism in several Cretaceous pterosaur lineages was made possible through body density reduction by expansion of the pulmonary air sac system throughout the trunk and the distal limb girdle skeleton, highlighting the importance of respiratory adaptations in pterosaur evolution, and the dramatic effect of the release of physical constraints on morphological diversification and evolutionary radiation.

Superfluid helium on on-orbit transfer (SHOOT) flight experiment

International Nuclear Information System (INIS)

DiPirro, M.J.; Kittel, P.

1988-01-01

The SHOOT flight demonstration is being undertaken to verify component and system level technology necessary to resupply large superfluid helium dewars in space. The baseline configuration uses two identical 210 liter dewars connected by a transfer line which contains a quick disconnect coupling. The helium is transferred back and forth between the dewars under various conditions of flow rate, parasitic heat load, and temperature. An astronaut Extra-Vehicular Activity is also planned to manually mate and demate the coupling. The components necessary for the flight and currently being developed are described

Short outlines of books by Estonian authors / Janika Kronberg, Rutt Hinrikus

Index Scriptorium Estoniae

Kronberg, Janika, 1963-

2006-01-01

Arvustus: Krull, Hasso. Loomise mõnu ja kiri. Tallinn : Kultuurileht, 2006 ; Aleksejev, Tiit. Valge kuningriik. Tallinn : Varrak, 2006 ; Baturin, Nikolai. Sõnajalg kivis. Tallinn : Eesti Raamat, 2006 ; Nõu, Helga. Ood lastud rebasele. Tallinn : Eesti Keele Sihtasutus, 2006 ; Kaus, Jan. Tema. Tallinn : Tuum, 2006 ; Krull, Hasso. Talv. Tallinn : Tuum, 2006 ; Soomets, Triin. Väljas. Tallinn : Tuum, 2006 ; Kareva, Doris. Aja kuju. Tallinn : Verb, 2006 ; Vint, Toomas. Topeltvalguses. Tallinn : Eesti Keele Sihtasutus, 2005 ; Bristol, Piret. Sõud. Tallinn : Eesti Keele Sihtasutus, 2005 ; Valton, Arvo. Taltsutatud lammas : jutud. Tallinn : Kirjastuskeskus, 2005 ; Kivastik, Mart. Külmetava kunstniku portreed. Viinistu triloogia. Tartu : Väike Öömuusika, 2006

Short outlines of books by Estonian authors / Janika Kronberg, Rutt Hinrikus

Index Scriptorium Estoniae

Kronberg, Janika, 1963-

2004-01-01

Tutvustus: Talvik, Heiti. Legendaarne. Tartu : Ilmamaa, 2004 ; Pilter, Lauri. Lohejas pilv : romaan lühijuttudes. Tallinn : Tuum, 2004 ; Raud, Rein. Hector ja Bernard. Tallinn : Tuum, 2004 ; Ruben, Aarne. Elajas trepi eelastmel. Tallinn : Tuum, 2004 ; fs. 2004. Tallinn : Tuum, 2004 ; Normet, Dagmar. ...ainult võti taskus. Tallinn : Varrak, 2004 ; Künnap, Asko. Ja sisalikud vastasid (kolmes kirjas). Tallinn : Näo Kirik, 2003 ; Kall, Toomas. Armas aeg. Tallinn : Tänapäev, 2004 ; Õunapuu, Ervin. Eesti gootika II. Tallinn : Umara, 2004 ; Soomets, Triin. Leping number 2 : luuletusi 2000-2003. Tallinn : Tuum, 2004 ; Tuulik, Jüri. Linnusita : [jutustused, lühijutud, näidendid ja vested]. Tallinn : Maalehe Raamat, 2004 ; Raudam, Toomas. Teie. Tallinn : Eesti Keele Sihtasutus, 2003 ; Härm, Viiu. Keegi teeline : luuletused. Tallinn : Varrak, 2004 ; Härm, Viiu. Õhuaken : romaan. Tallinn : Varrak, 2004

AMS Ground Truth Measurements: Calibration and Test Lines

International Nuclear Information System (INIS)

Wasiolek, P.

2013-01-01

Airborne gamma spectrometry is one of the primary techniques used to define the extent of ground contamination after a radiological incident. Its usefulness was demonstrated extensively during the response to the Fukushima nuclear power plant (NPP) accident in March-May 2011. To map ground contamination a set of scintillation detectors is mounted on an airborne platform (airplane or helicopter) and flown over contaminated areas. The acquisition system collects spectral information together with the aircraft position and altitude every second. To provide useful information to decision makers, the count rate data expressed in counts per second (cps) needs to be converted to the terrestrial component of the exposure rate 1 m above ground, or surface activity of isotopes of concern. This is done using conversion coefficients derived from calibration flights. During a large scale radiological event, multiple flights may be necessary and may require use of assets from different agencies. However, as the production of a single, consistent map product depicting the ground contamination is the primary goal, it is critical to establish very early into the event a common calibration line. Such a line should be flown periodically in order to normalize data collected from different aerial acquisition systems and potentially flown at different flight altitudes and speeds. In order to verify and validate individual aerial systems, the calibration line needs to be characterized in terms of ground truth measurements. This is especially important if the contamination is due to short-lived radionuclides. The process of establishing such a line, as well as necessary ground truth measurements, is described in this document.

AMS Ground Truth Measurements: Calibrations and Test Lines

Energy Technology Data Exchange (ETDEWEB)

Wasiolek, Piotr T. [National Security Technologies, LLC

2015-12-01

Airborne gamma spectrometry is one of the primary techniques used to define the extent of ground contamination after a radiological incident. Its usefulness was demonstrated extensively during the response to the Fukushima NPP accident in March-May 2011. To map ground contamination, a set of scintillation detectors is mounted on an airborne platform (airplane or helicopter) and flown over contaminated areas. The acquisition system collects spectral information together with the aircraft position and altitude every second. To provide useful information to decision makers, the count data, expressed in counts per second (cps), need to be converted to a terrestrial component of the exposure rate at 1 meter (m) above ground, or surface activity of the isotopes of concern. This is done using conversion coefficients derived from calibration flights. During a large-scale radiological event, multiple flights may be necessary and may require use of assets from different agencies. However, because production of a single, consistent map product depicting the ground contamination is the primary goal, it is critical to establish a common calibration line very early into the event. Such a line should be flown periodically in order to normalize data collected from different aerial acquisition systems and that are potentially flown at different flight altitudes and speeds. In order to verify and validate individual aerial systems, the calibration line needs to be characterized in terms of ground truth measurements This is especially important if the contamination is due to short-lived radionuclides. The process of establishing such a line, as well as necessary ground truth measurements, is described in this document.

How Theories of Perception Deploy the Line: Reconfiguring Students' Bodies through Topo-Philosophy

Science.gov (United States)

de Freitas, Elizabeth

2014-01-01

In this essay Elizabeth de Freitas follows Tim Ingold's groundbreaking anthropological work on lines and their cultural and material significance to argue that the line is the engine of theory, be it the drawn line of inscription or mathematical measure, the exclusionary line of delineation, or the undulating generative line of flight. De…

Method and System for Weakening Shock Wave Strength at Leading Edge Surfaces of Vehicle in Supersonic Atmospheric Flight

Science.gov (United States)

Daso, Endwell O. (Inventor); Pritchett, Victor E., II (Inventor); Wang, Ten-See (Inventor); Farr, Rebecca Ann (Inventor); Auslender, Aaron Howard (Inventor); Blankson, Isaiah M. (Inventor); Plotkin, Kenneth J. (Inventor)

2015-01-01

A method and system are provided to weaken shock wave strength at leading edge surfaces of a vehicle in atmospheric flight. One or more flight-related attribute sensed along a vehicle's outer mold line are used to control the injection of a non-heated, non-plasma-producing gas into a local external flowfield of the vehicle from at least one leading-edge surface location along the vehicle's outer mold line. Pressure and/or mass flow rate of the gas so-injected is adjusted in order to cause a Rankine-Hugoniot Jump Condition along the vehicle's outer mold line to be violated.

Short outlines of books by Estonian authors / Brita Melts, Rutt Hinrikus, Maret Vaher and Arno Oja

Index Scriptorium Estoniae

Melts, Brita

2014-01-01

Arvustus: Kronberg, Janika. Rännud kuue teejuhiga. Tallinn : Go Group, 2013 ; Kallaste, Helen. Kogutud hetked. Tallinn : Verb, 2012 ; Ahi, Eda. Gravitatsioon. Tallinn : Verb, 2013 ; Heinsaar, Mehis. Ülikond. Tallinn : Menu Kirjastus, 2013 ; Kann, Kaja. Eratee. Tallinn : Hea Lugu, 2013 ; Kivirähk, Andrus. Maailma otsas. Tallinn : Eesti Keele Sihtasutus, 2013 ; Kurvitz, Robert. Püha ja õudne lõhn. Tallinn : ZA/UM, 2013 ; Mattheus, Ülo. Tema salajane palve. Tallinn : Tuum, 2013 ; Kangro, Maarja. Dantelik auk. Tallinn : Eesti Keele Sihtasutus, 2012

Short outlines of books by Estonian authors / Brita Melts, Rutt Hinrikus and Janika Kronberg

Index Scriptorium Estoniae

Melts, Brita

2013-01-01

Arvustus: Baturin, Nikolai. Lendav hollandlanna. Tallinn : Eesti Raamat, 2012 ; Friedenthal, Meelis. Mesilased. Tallinn : Varrak, 2012 ; Kaus, Jan. Koju. Tallinn : Tuum, 2012 ; Kaldmaa, Kätlin. Armastuse tähestik. Tallinn : NyNorden, 2012 ; Kivastik, Mart. Vietnami retsept. Tartu : Väike Öömuusika, 2012 ; Õnnepalu, Tõnu. Kuidas on elada. Tallinn : Varrak, 2012 ; Õnnepalu, Tõnu. Mandala. Tallinn : Varrak, 2012 ; Riismaa, Kaur. Rebase matmine. Tallinn : Näo Kirik, 2012 ; Vadi, Urmas. Tagasi Eestisse. Saarde-Pärnu : Jumalikud Ilmutused, 2012 ; Vint, Toomas. Avalikult abielust. Tallinn : Tulikiri, 2012 ; Kangro, Maarja. Dantelik auk. Tallinn : Eesti Keele Sihtasutus, 2012 ; Kaevats, Mihkel. Ungari kirsid & teisi luuletusi. Tallinn : Pegasus, 2012.

Hybrid Adaptive Flight Control with Model Inversion Adaptation

Science.gov (United States)

Nguyen, Nhan

2011-01-01

This study investigates a hybrid adaptive flight control method as a design possibility for a flight control system that can enable an effective adaptation strategy to deal with off-nominal flight conditions. The hybrid adaptive control blends both direct and indirect adaptive control in a model inversion flight control architecture. The blending of both direct and indirect adaptive control provides a much more flexible and effective adaptive flight control architecture than that with either direct or indirect adaptive control alone. The indirect adaptive control is used to update the model inversion controller by an on-line parameter estimation of uncertain plant dynamics based on two methods. The first parameter estimation method is an indirect adaptive law based on the Lyapunov theory, and the second method is a recursive least-squares indirect adaptive law. The model inversion controller is therefore made to adapt to changes in the plant dynamics due to uncertainty. As a result, the modeling error is reduced that directly leads to a decrease in the tracking error. In conjunction with the indirect adaptive control that updates the model inversion controller, a direct adaptive control is implemented as an augmented command to further reduce any residual tracking error that is not entirely eliminated by the indirect adaptive control.

Mitmekülgne eesti lastekirjandus [2006. a.] / Jaanika Palm

Index Scriptorium Estoniae

Palm, Jaanika, 1973-

2008-01-01

Arvustus: Tungal, Leelo. Lätikeelne jäätis ja teisi luuletusi. Tallinn : Tuum, 2006 ; Trull, Ilmar. Musta kassi mumba. Tallinn : Eesti Ekspressi Kirjastus, 2006 ; Wimberg. Põngerjate laulud. Tallinn : Varrak, 2006 ; Muidugi, Eino. Lõbus pere ütleb tere! Tallinn : Koolibri, 2006 ; Nemvalts, Urmas. Väikeste meeste jutud. [Tallinn] : Grenader, 2006 ; Kangro, Maarja, Kangro, Kirke. Puuviljadraakon. Tallinn : Koolibri, 2006 ; Kilkson, Tiina. Pisikese Peetri pikk pühapäev. Tallinn : Koolibri, 2006 ; Pelmas, Elsa. Sussipäkapikk Siisi seiklused. Tallinn : TEA Kirjastus, 2006 ; Sauter, Peeter. Laiskade laste raamat. Tallinn : Huma, 2006 ; Kivirähk, Andrus. Leiutajateküla Lotte. Tallinn : Eesti Joonisfilm, 2006 ; Ulman, Mihkel. Nukkude teater. Tartu : Elmatar, 2006 ; Rannap, Jaan. Roheline kindlus. Tallinn : Tiritamm, 2006 ; Vallik, Aidi. Narkohollo ehk Florose vabastamine. Haapsalu : Lugu-Loo, 2006 ; Leesalu, Diana. Mängult on päriselt. Tallinn : Tänapäev, 2006 ; Laidla, Siiri. Pärnaõietee. Tallinn : Canopus, 2006

Mitmekülgne eesti lastekirjandus [2006. a.] / Jaanika Palm

Index Scriptorium Estoniae

Palm, Jaanika, 1973-

2007-01-01

Arvustus: Tungal, Leelo. Lätikeelne jäätis ja teisi luuletusi. Tallinn : Tuum, 2006 ; Trull, Ilmar. Musta kassi mumba. Tallinn : Eesti Ekspressi Kirjastus, 2006 ; Wimberg. Põngerjate laulud. Tallinn : Varrak, 2006 ; Muidugi, Eino. Lõbus pere ütleb tere! Tallinn : Koolibri, 2006 ; Nemvalts, Urmas. Väikeste meeste jutud. [Tallinn] : Grenader, 2006 ; Kangro, Maarja, Kangro, Kirke. Puuviljadraakon. Tallinn : Koolibri, 2006 ; Kilkson, Tiina. Pisikese Peetri pikk pühapäev. Tallinn : Koolibri, 2006 ; Pelmas, Elsa. Sussipäkapikk Siisi seiklused. Tallinn : TEA Kirjastus, 2006 ; Sauter, Peeter. Laiskade laste raamat. Tallinn : Huma, 2006 ; Kivirähk, Andrus. Leiutajateküla Lotte. Tallinn : Eesti Joonisfilm, 2006 ; Ulman, Mihkel. Nukkude teater. Tartu : Elmatar, 2006 ; Rannap, Jaan. Roheline kindlus. Tallinn : Tiritamm, 2006 ; Vallik, Aidi. Narkohollo ehk Florose vabastamine. Haapsalu : Lugu-Loo, 2006 ; Leesalu, Diana. Mängult on päriselt. Tallinn : Tänapäev, 2006 ; Laidla, Siiri. Pärnaõietee. Tallinn : Canopus, 2006

Initial Flight Test of the Production Support Flight Control Computers at NASA Dryden Flight Research Center

Science.gov (United States)

Carter, John; Stephenson, Mark

1999-01-01

The NASA Dryden Flight Research Center has completed the initial flight test of a modified set of F/A-18 flight control computers that gives the aircraft a research control law capability. The production support flight control computers (PSFCC) provide an increased capability for flight research in the control law, handling qualities, and flight systems areas. The PSFCC feature a research flight control processor that is "piggybacked" onto the baseline F/A-18 flight control system. This research processor allows for pilot selection of research control law operation in flight. To validate flight operation, a replication of a standard F/A-18 control law was programmed into the research processor and flight-tested over a limited envelope. This paper provides a brief description of the system, summarizes the initial flight test of the PSFCC, and describes future experiments for the PSFCC.

Data acquisition system for a positron tomograph using time-of-flight information

International Nuclear Information System (INIS)

Bertin, Francois.

1981-12-01

Progress in nuclear instrumentation has led to the development of scintillators much faster than the NaI crystal traditionally used in nuclear medicine. As a result it is now possible to measure time-of-flight, i.e. the time between the arrival of two γ rays emitted in coincidence on two detectors. With this extra information the β + annihilation site may be located. The introduction of time-of-flight in tomographic techniques called for research along two lines: - ''theoretical'' research leading to the creation of a new image reconstruction algorithm taking into account time-of-flight information - applied research leading to the development of an efficient measurement line and sophisticated data acquisition and processing electronics. This research has been carried out at LETI and is briefly outlined in chapter I. Chapter II shows how the introduction of time-of-flight and the modification of the reconstruction algorithm complicate the electronic and informatic equipment of the tomograph. Several acquisition and processing strategies are proposed, then the need to use an intermediate mass storage and hence to design a complex acquisition operator is demonstrated. Chapter III examines the structure of the acquisition operator and the resulting block diagram is presented in detail in chapter IV [fr

Short outlines of books by Estonian authors / Janika Kronberg, Rutt Hinrikus

Index Scriptorium Estoniae

Kronberg, Janika, 1963-

2008-01-01

Arvustus: Kareva, Doris. Lõige. Tallinn : Verb, 2007 ; Õnnepalu, Tõnu. Flandria päevik. Tallinn : Varrak, 2007 ; Mihkelson, Ene. Katkuhaud. Tallinn : Varrak, 2007 ; Vint, Toomas. Mäluauguga naine. Tallinn : Eesti Keele Sihtasutus, 2007 ; Pervik, Aino. Suleline, Puhuja ja must munk. Tallinn : Tänapäev, 2007 ; Mutt, Mihkel. Siseemigrant. Novellid Rui taevalike kommentaaridega. Tallinn : Fabian, 2007 ; Nõlvak, Valentine. Ellujääja mälestused. Tallinn : Varrak, 2007 ; Tungal, Leelo. Täisminevik. Tallinn : Tänapäev, 2007 ; Kangro, Maarja. Tule mu koopasse, mateeria. Tallinn : Eesti Keele Sihtasutus, 2007

Short Outlines of Books by Estonian Authors / Janika Kronberg, Rutt Hinrikus

Index Scriptorium Estoniae

Kronberg, Janika, 1963-

2009-01-01

Arvustus: Karusoo, Merle. Kui ruumid on täis : Eesti rahva elulood teatritekstides 1982-2005. Tallinn : Varrak, 2008 ; Aleksejev, Tiit. Palveränd. Tallinn : Varrak, 2008 ; Saat, Mari. Lasnamäe lunastaja. Tallinn : Tuum, 2008 ; Tarand, Mari. Ajapildi sees. Tartu : Ilmamaa, 2008 ; Ojamaa, Liisi. Jõgi asfaldi all. Tallinn : Varrak, 2008 ; Kaalep, Ain. Muusad ja maastikud. Luuletused aastaist 1945-2008. Tallinn : Tänapäev, 2008 ; Toona, Elin. Ella. Tallinn : Kultuurileht, 2008 ; Hellerma, Kärt. Sinine missa. Valik reisikirju. Tallinn : Tuum, 2008 ; Raud, Rein. Vend. Tallinn : Tuum, 2008 ; Kruusa, Kalju. Pilvedgi mindgi liigutavadgi. Tallinn : Koma, 2008

Methodologies for Improving Flight Project Information Capture, Storage, and Dissemination

Science.gov (United States)

Equils, Douglas J.

2011-01-01

This paper will discuss the drawbacks and risks of the current documentation paradigm, how Document QuickStart improves on that process and ultimately how this stream-lined approach will reduce risk and costs to the next generation of Flight Projects at JPL

Recursive subspace identification for in flight modal analysis of airplanes

OpenAIRE

De Cock , Katrien; Mercère , Guillaume; De Moor , Bart

2006-01-01

International audience; In this paper recursive subspace identification algorithms are applied to track the modal parameters of airplanes on-line during test flights. The ability to track changes in the damping ratios and the influence of the forgetting factor are studied through simulations.

Short Outlines of Books by Estonian authors / Rutt Hinrikus

Index Scriptorium Estoniae

Hinrikus, Rutt, 1946-

2007-01-01

Tutvustus: Miljutina, Tamara. Inimesed minu elus. Tallinn : Varrak, 2007 ; Soosaar, Enn. Isa ja aeg. Tallinn : Kultuurileht, 2007. (Loomingu Raamatukogu ; 5) ; Paju, Imbi. Tõrjutud mälestused. Tallinn : Eesti Entsüklopeediakirjastus, 2007 ; Kaplinski, Jaan. Seesama jõgi. Tallinn : Vagabund, 2007 ; Laanem, Tiina. Väikesed vanamehed. Tallinn : Eesti Päevalehe Kirjastus, 2007 ; Vaarandi, Debora. Aastad ja päevad. Tallinn : Tänapäev, 2006 ; Berg, Maimu. Unustatud inimesed. Tallinn : Tuum, 2007 ; Heinsaar, Mehis. Rändaja õnn. Tallinn : Verb, 2007

Short outlines of books by Estonian authors / Janika Kronberg, Rutt Hinrikus

Index Scriptorium Estoniae

Kronberg, Janika, 1963-

2004-01-01

Tutvustus: Baturin, Nikolai. Kentaur. Tallinn : Eesti Raamat, 2003 ; Kaplinski, Jaan. Isale. Tallinn : Varrak, 2003 ; Jaks, Ilmar. Pimedus. Tartu : Ilmamaa, 2003 ; Ivask, Ivar. Tähtede tähendust tunda. Tartu : Ilmamaa, 2003 ; Vint, Toomas. Minu abielu prostituudiga. Tallinn : Eesti Keele Sihtasutus, 2003 ; Ehin, Kristiina. Luigeluulinn. Tallinn : Huma, 2004 ; Kivisildnik. Päike, mida sa õhtul teed? Tallinn : Perioodika, 2003 ; Kivisildnik. Rahvuseepos Kalevipoeg ehk armastus. Tallinn : Tuum, 2003 ; Veidemann, Rein. Lastekodu. Tallinn : Eesti Keele Sihtasutus, 2003 ; Park, Eeva. Lõks lõpmatuses. Tallinn : Tänapäev, 2003 ; Traat, Mats. Islandi suvi. Tartu : Ilmamaa, 2003 ; Kauksi Ülle. Uibu. Tartu : Kauksi Ülle Mänedsment, 2003 ; Kross, Jaan. Kallid kaasteelised. Tallinn : Eesti Keele Sihtasutus, 2003 ; Undusk, Jaan. Quevedo. Tallinn : Perioodika, 2003

Short outlines of books by Estonian authors / Janika Kronberg, Rutt Hinrikus

Index Scriptorium Estoniae

Kronberg, Janika, 1963-

2008-01-01

Arvustus: Afanasjev, Vahur. Kosmos. Tallinn : Jutulind, 2008 ; Hvostov, Andrei. Võõrad lood. Tallinn : Tänapäev, 2008 ; Lauli, Olle. Niguliste õpilased. Tallinn : Verb, 2007 ; Rooste, Jürgen. Tavaline eesti idioot. Pärnu : Ji, 2008 ; Talvet, Jüri. Silmad peksavad une seinu. Tartu : Ilmamaa, 2008 ; Beekman, Aimée. Proovielu. Tallinn : Varrak, 2008 ; Kivi, Aita. Lähedal. Tallinn : Ajakirjade Kirjastus, 2008 ; Beekman, Vladimir. Alles see oli. Tallinn : Tänapäev, 2008 ; Viiding, Elo. Püha Maama. Tallinn : Tuum, 2008 ; Nõu, Helga. Peaaegu geenius ehk Schrödingeri kassi otsimas. Tallinn : Atlex, 2008 ; Unt, Lii. Parim näitleja linnas. Varanasi päevaraamat. Tallinn : Eesti Ekspressi Kirjastus, 2007 ; Sild, Ivar. Tantsiv linn. Tallinn : Tuum, 2007

Tõhusad tükid teismeliste poiste raamaturiiulis / Aidi Vallik

Index Scriptorium Estoniae

Vallik, Aidi, 1971-

2007-01-01

Tutvustus: Townsend, Sue. Salajane päevik. Tallinn : Tänapäev, 2002 ; Jacobsson, Anders, Olsson, Sören. Emanuel. Tallinn : Hotger, 2002 ; Brennan, Herbie. Haldjasõjad. Tallinn : Varrak, 2005 ; Paolini, Christopher. Eragon. Tallinn : Pegasus, 2005 ; Paolini, Christopher. Vanem. Tallinn : Pegasus, 2006 ; Vallik, Aidi. Narkohollo ehk Florose vabastamine. Tartu : Lugu-Loo, 2006 ; Schlüter, Andreas. Laste linn. Tallinn : Tormikiri, 2005 ; Schlüter, Andreas. Rööv. Tallinn : Tormikiri, 2005 ; Sachar, Lois. Augud. Tallinn : Draakon ja Kuu, 2005 ; Rannap, Jaan. Roheline kindlus. Tartu : Tiritamm, 2006 ; Henno, Sass. Mina olin siin. Tallinn : Eesti Päevalehe Kirjastus, 2005

Metabolite profiling of a diverse collection of wheat lines using ultraperformance liquid chromatography coupled with time-of-flight mass spectrometry.

Directory of Open Access Journals (Sweden)

Shawna B Matthews

Full Text Available Genetic differences among major types of wheat are well characterized; however, little is known about how these distinctions affect the small molecule profile of the wheat seed. Ethanol/water (65% v/v extracts of seed from 45 wheat lines representing 3 genetically distinct classes, tetraploid durum (Triticum turgidum subspecies durum (DW and hexaploid hard and soft bread wheat (T. aestivum subspecies aestivum (BW were subjected to ultraperformance liquid chromatography coupled with time-of-flight mass spectrometry (UPLC-TOF-MS. Discriminant analyses distinguished DW from BW with 100% accuracy due to differences in expression of nonpolar and polar ions, with differences attributed to sterol lipids/fatty acids and phospholipids/glycerolipids, respectively. Hard versus soft BW was distinguished with 100% accuracy by polar ions, with differences attributed to heterocyclic amines and polyketides versus phospholipid ions, respectively. This work provides a foundation for identification of metabolite profiles associated with desirable agronomic and human health traits and for assessing how environmental factors impact these characteristics.

Seitse raamatut ühtmoodi loodusest, kuid kõik erinevad / Ulvar Käärt, Mari Klein

Index Scriptorium Estoniae

Käärt, Ulvar, 1982-

2009-01-01

Arvustus: Järva, Jaanus. Looduse aasta. Tallinn : Varrak, 2008; Järva, Jaanus. Raba : vaikuses ja varjus. Tallinn : Pegasus, 2008; Savisaar, Remo. Loodus kutsub. Tallinn : Varrak, 2008; Relve, Hendrik. Eesti looduse vägi. Tallinn : Koolibri, 2008; Tartes, Urmas, Põder, Jaak. Legendiloomad. Tallinn : Varrak, 2008; Eesti maastikud. Tallinn : Tänapäev, 2008; Veedla, Peep. Lindudega sõbraks / pildid joonistanud Triinu Ootsing. Tallinn : Berit Grupp, 2008

Short outlines of books by Estonian authors / Brita Melts, Rutt Hinrikus and Janika Kronberg

Index Scriptorium Estoniae

Melts, Brita

2012-01-01

Arvustus: Helme, Peeter. Varastatud aja lõpus. Tallinn : Tuum, 2011 ; Jõerüüt, Jaak. Kõik luuletused. Tallinn : Eesti Keele Sihtasutus, 2011 ; Kareva, Doris. Sa pole üksi. Tallinn : Verb, 2011 ; Paju, Imbi. Soome lahe õed : vaadates teiste valu. Tallinn : Hea lugu, 2011 ; Pervik, Aino. Matlena teekond. Tallinn : Mustvalge Kirjastus, 2010 ; Raud, Rein. Hotell Amalfi. Tallinn : Tuum, 2011 ; Sommer, Lauri. Räestu raamat. Tallinn : Menu Kirjastus, 2012 ; Kasemaa. Andrus. Leskede kadunud maailm. Tallinn : Varrak, 2012 ; Teede, Andra. Käigud. Pärnu : Jumalikud Ilmutused, 2011

Estonian authors / Janika Kronberg, Rutt Hinrikus

Index Scriptorium Estoniae

Kronberg, Janika, 1963-

2007-01-01

Tutvustus: Mattheus, Ülo.¡India armastus. Tallinn : Eesti Keele Sihtasutus, 2006 ;¡Teder,¡Tarmo. Onanistid. Tallinn :¡Tuum, 2006 ;¡Hirv, Indrek. Surmapõletaja. Tallinn :¡Tuum, 2006 ;¡Hvostov, Andrei. Henrik : näidend 12-s pildis. Tallinn : Kultuurileht, 2006. (Loomingu Raamatukogu ;¡20) ;¡Traat,¡Mats. Naised ja pojad. Tallinn : Looming, 2006, nr. 2-5 ;¡Traat, Mats. Sarviku armastus. Tallinn :¡Looming, 2006, nr. 11 ;¡Kaardipakk II. Tallinn : Näo Kirik, 2006 ;¡Kivirähk,¡Andrus. Mees, kes teadis ussisõnu. Tallinn :¡Eesti Keele Sihtasutus, 2007 ;¡Õunapuu,¡Ervin. Meie igapäevane jää :¡eesti gootika III. Tallinn : Varrak, 2006 ;¡Ehlvest, Jüri. Palverännak. Tallinn :¡Tuum, 2005

In-Flight Sleep of Flight Crew During a 7-hour Rest Break: Implications for Research and Flight Safety

Science.gov (United States)

Signal, T. Leigh; Gander, Philippa H.; van den Berg, Margo J.; Graeber, R. Curtis

2013-01-01

Study Objectives: To assess the amount and quality of sleep that flight crew are able to obtain during flight, and identify factors that influence the sleep obtained. Design: Flight crew operating flights between Everett, WA, USA and Asia had their sleep recorded polysomnographically for 1 night in a layover hotel and during a 7-h in-flight rest opportunity on flights averaging 15.7 h. Setting: Layover hotel and in-flight crew rest facilities onboard the Boeing 777-200ER aircraft. Participants: Twenty-one male flight crew (11 Captains, mean age 48 yr and 10 First Officers, mean age 35 yr). Interventions: N/A. Measurements and Results: Sleep was recorded using actigraphy during the entire tour of duty, and polysomnographically in a layover hotel and during the flight. Mixed model analysis of covariance was used to determine the factors affecting in-flight sleep. In-flight sleep was less efficient (70% vs. 88%), with more nonrapid eye movement Stage 1/Stage 2 and more frequent awakenings per h (7.7/h vs. 4.6/h) than sleep in the layover hotel. In-flight sleep included very little slow wave sleep (median 0.5%). Less time was spent trying to sleep and less sleep was obtained when sleep opportunities occurred during the first half of the flight. Multivariate analyses suggest age is the most consistent factor affecting in-flight sleep duration and quality. Conclusions: This study confirms that even during long sleep opportunities, in-flight sleep is of poorer quality than sleep on the ground. With longer flight times, the quality and recuperative value of in-flight sleep is increasingly important for flight safety. Because the age limit for flight crew is being challenged, the consequences of age adversely affecting sleep quantity and quality need to be evaluated. Citation: Signal TL; Gander PH; van den Berg MJ; Graeber RC. In-flight sleep of flight crew during a 7-hour rest break: implications for research and flight safety. SLEEP 2013;36(1):109–115. PMID:23288977

A Scalable Semantics-Based Verification System for Flight Critical Software, Phase II

Data.gov (United States)

National Aeronautics and Space Administration — Flight-critical systems rely on an ever increasing amount of software—the Boe- ing 777 contains over 2 million lines of code. Most of this code is written in the C...

In-flight sleep of flight crew during a 7-hour rest break: implications for research and flight safety.

Science.gov (United States)

Signal, T Leigh; Gander, Philippa H; van den Berg, Margo J; Graeber, R Curtis

2013-01-01

To assess the amount and quality of sleep that flight crew are able to obtain during flight, and identify factors that influence the sleep obtained. Flight crew operating flights between Everett, WA, USA and Asia had their sleep recorded polysomnographically for 1 night in a layover hotel and during a 7-h in-flight rest opportunity on flights averaging 15.7 h. Layover hotel and in-flight crew rest facilities onboard the Boeing 777-200ER aircraft. Twenty-one male flight crew (11 Captains, mean age 48 yr and 10 First Officers, mean age 35 yr). N/A. Sleep was recorded using actigraphy during the entire tour of duty, and polysomnographically in a layover hotel and during the flight. Mixed model analysis of covariance was used to determine the factors affecting in-flight sleep. In-flight sleep was less efficient (70% vs. 88%), with more nonrapid eye movement Stage 1/Stage 2 and more frequent awakenings per h (7.7/h vs. 4.6/h) than sleep in the layover hotel. In-flight sleep included very little slow wave sleep (median 0.5%). Less time was spent trying to sleep and less sleep was obtained when sleep opportunities occurred during the first half of the flight. Multivariate analyses suggest age is the most consistent factor affecting in-flight sleep duration and quality. This study confirms that even during long sleep opportunities, in-flight sleep is of poorer quality than sleep on the ground. With longer flight times, the quality and recuperative value of in-flight sleep is increasingly important for flight safety. Because the age limit for flight crew is being challenged, the consequences of age adversely affecting sleep quantity and quality need to be evaluated.

Lugupeetud emakeeleõpetaja! / Martin Ehala

Index Scriptorium Estoniae

Ehala, Martin, 1963-

2006-01-01

Tutvustatakse eesti keele õpikuid: Ehala, Martin. Eesti keele struktuur. Tallinn, 2001 ; Ehala, Martin. Kirjutamise kunst. Tallinn, 2000 ; Ehala, Martin. Eesti kirjakeel. Tallinn, 2002 ; Madisso, Maia. Keele- ja tekstiharjutusi abiturientidele. Tallinn, 2002 ; Ehala, Martin ; Veismann, Tiina jt. Noor keelekasutaja. Tallinn, 2005

Strapdown Airborne Gravimetry Quality Assessment Method Based on Single Survey Line Data: A Study by SGA-WZ02 Gravimeter

Science.gov (United States)

Wu, Meiping; Cao, Juliang; Zhang, Kaidong; Cai, Shaokun; Yu, Ruihang

2018-01-01

Quality assessment is an important part in the strapdown airborne gravimetry. Root mean square error (RMSE) evaluation method is a classical way to evaluate the gravimetry quality, but classical evaluation methods are preconditioned by extra flight or reference data. Thus, a method, which is able to largely conquer the premises of classical quality assessment methods and can be used in single survey line, has been developed in this paper. According to theoretical analysis, the method chooses the stability of two horizontal attitude angles, horizontal specific force and vertical specific force as the determinants of quality assessment method. The actual data, collected by SGA-WZ02 from 13 flights 21 lines in certain survey, was used to build the model and elaborate the method. To substantiate the performance of the quality assessment model, the model is applied in extra repeat line flights from two surveys. Compared with internal RMSE, standard deviation of assessment residuals are 0.23 mGal and 0.16 mGal in two surveys, which shows that the quality assessment method is reliable and stricter. The extra flights are not necessary by specially arranging the route of flights. The method, summarized from SGA-WZ02, is a feasible approach to assess gravimetry quality using single line data and is also suitable for other strapdown gravimeters. PMID:29373535

The re-flight of the Colorado high-resolution Echelle stellar spectrograph (CHESS): improvements, calibrations, and post-flight results

Science.gov (United States)

Hoadley, Keri; France, Kevin; Kruczek, Nicholas; Fleming, Brian; Nell, Nicholas; Kane, Robert; Swanson, Jack; Green, James; Erickson, Nicholas; Wilson, Jacob

2016-07-01

In this proceeding, we describe the scientific motivation and technical development of the Colorado High- resolution Echelle Stellar Spectrograph (CHESS), focusing on the hardware advancements and testing supporting the second flight of the payload (CHESS-2). CHESS is a far ultraviolet (FUV) rocket-borne instrument designed to study the atomic-to-molecular transitions within translucent cloud regions in the interstellar medium (ISM). CHESS is an objective f/12.4 echelle spectrograph with resolving power > 100,000 over the band pass 1000 - 1600 Å. The spectrograph was designed to employ an R2 echelle grating with "low" line density. We compare the FUV performance of experimental echelle etching processes (lithographically by LightSmyth, Inc. and etching via electron-beam technology by JPL Microdevices Laboratory) with traditional, mechanically-ruled gratings (Bach Research, Inc. and Richardson Gratings). The cross-dispersing grating, developed and ruled by Horiba Jobin-Yvon, is a holographically-ruled, "low" line density, powered optic with a toroidal surface curvature. Both gratings were coated with aluminum and lithium fluoride (Al+LiF) at Goddard Space Flight Center (GSFC). Results from final efficiency and reflectivity measurements for the optical components of CHESS-2 are presented. CHESS-2 utilizes a 40mm-diameter cross-strip anode readout microchannel plate (MCP) detector fabricated by Sensor Sciences, Inc., to achieve high spatial resolution with high count rate capabilities (global rates 1 MHz). We present pre-flight laboratory spectra and calibration results. CHESS-2 launched on 21 February 2016 aboard NASA/CU sounding rocket mission 36.297 UG. We observed the intervening ISM material along the sightline to epsilon Per and present initial characterization of the column densities, temperature, and kinematics of atomic and molecular species in the observation.

Flight Tests of a 0.13-Scale Model of the Convair XFY-1 Vertically Rising Airplane in a Setup Simulating that Proposed for Captive-Flight Tests in a Hangar, TED No. NACA DE 368

Science.gov (United States)

Lovell, Powell M., Jr.

1953-01-01

An experimental investigation has been conducted to determine the dynamic stability and control characteristics of a 0.13-scale free-flight model of the Convair XFY-1 airplane in test setups representing the setup proposed for use in the first flight tests of the full-scale airplane in the Moffett Field airship hangar. The investigation was conducted in two parts: first, tests with the model flying freely in an enclosure simulating the hangar, and second, tests with the model partially restrained by an overhead line attached to the propeller spinner and ground lines attached to the wing and tail tips. The results of the tests indicated that the airplane can be flown without difficulty in the Moffett Field airship hangar if it does not approach too close to the hangar walls. If it does approach too close to the walls, the recirculation of the propeller slipstream might cause sudden trim changes which would make smooth flight difficult for the pilot to accomplish. It appeared that the tethering system proposed by Convair could provide generally satisfactory restraint of large-amplitude motions caused by control failure or pilot error without interfering with normal flying or causing any serious instability or violent jerking motions as the tethering lines restrained the model.

First Results of the aerogravity measurements during the geoscientific flight mission GEOHALO over Italy and the adjacent Mediterranean

Science.gov (United States)

Heyde, Ingo; Barthelmes, Franz; Scheinert, Mirko

2013-04-01

In June 2012 the first scientific flight mission was realized with the new German research aircraft HALO (High Altitude and Long Range Research Aircraft). For this geoscientific flight mission GEOHALO was equipped with geophysical-geodetic instrumentation to acquire data over the tectonically active region of Italy and the adjacent Medtiterranean. The Federal Institute for Geosciences and Resources (BGR) as a member of the "HALO geoscience group" operated the recently modernized KSS32-M aerogravity system. The instrumentation of the group partners consists of an additional gravimeter, vector and scalar magnetometers, a laser altimeter and GNSS equipment with zenith, sideward and nadir antennas. During four flights with duration of up to 10 hours, data along a total track length of 16150 kilometers were obtained. The mission flights started and ended at the special airfield Oberpfaffenhofen, near the compound of the German Aerospace Center (DLR). Eight parallel profiles running from north-west to south-east were flown in an altitude of about 3500 m. The length of each profile was about 1000 km with a line spacing of 40 km. The flight velocity on the survey lines amounted to approximately 450 km/h. Four crossing lines of about 300 km length and a profile at an altitude of about 10500 m along the same track as a line in the lower altitude completed the survey. The first results of the BGR aerogravity will be presented. To determine the free-air gravity anomalies from the measured gravimeter data a number of corrections have to be applied. For their calculation mainly high-precision position and velocity data are mandatory. The kinematic GPS data were combined with INS data. In addition to own GPS base station data from Oberpfaffenhofen, data of Italian GNSS stations were considered to improve the determination of the flight trajectory by differential GPS. The corrected gravity data are compared with the corresponding data from global gravity models. The free

Short outlines of books by Estonian authors / Janika Kronberg, Rutt Hinrikus

Index Scriptorium Estoniae

Kronberg, Janika, 1963-

2003-01-01

Talvet, Jüri. ElegÍa Estonia y otros poemas = Eesti eleegia ja teisi luuletusi / Spanish transl. by the author and Albert L̉zaro Tinaut. Ciudad de València : Palmart, 2002 ; Ehlvest, Jüri. Hobune eikuskilt. Tallinn : Tänapäev, 2002 ; Raudam, Toomas. Saint-Prousti vastu. Tallinn : Eesti Keele Sihtasutus, 2002 ; Tode, Emil. Raadio. Tallinn : Eesti Keele Sihtasutus, 2002 ; Vene, Ilmar. Pahustumine ehk Uusaja olemus. Tallinn : Eesti Keele Sihtasutus, 2002 ; Annus, Epp. Kuidas kirjutada aega. Tallinn : Underi ja Tuglase Kirjanduskeskus, 2002 ; Lepik, Kalju. Valguse riie ei vanu. Kogutud luuletused 1938-1999 ; Barker, Matt. Waanenburgi tapatalgud. Tartu : EYS Veljesto, 2002 ; Kesküla, Kalev. Platoni riik. Tallinn : Tuum, 2002 ; Vahing, Vaino. Mängud ja kõnelused. Tallinn : Eesti Keele Sihtasutus, 2002 ; Tuulik, Jüri. Üksik lind mere kohal. Tallinn : Maalehe Raamat, 2002 ; Tätte, Jaan. Näidendid. Tallinn : Maalehe Raamat, 2002 ; Kareva, Doris. Mandragora. Tallinn : Huma, 2002

Short outlines of books by Estonian authors / Berk Vaher, Aare Pilv

Index Scriptorium Estoniae

Vaher, Berk, 1975-

2005-01-01

Tutvustus: Raudam, Toomas. Nips. Tallinn : Eesti Keele Sihtasutus, 2004 ; Ilus Armin : eesti lühiproosat 1987-2002 / koost. Udo Uibo. Tallinn : Varrak, 2004 ; Ehlvest, Jüri von. Rahuldus. Tartu : Ilukirjandus, 2004 ; Ki:wa. Roboti tee on nihe ; Salatühik. Tallinn : Eesti Kunstimuuseum, 2004 ; Sommer, Lauri. Nõidade õrnus. Sännä : Tiivaalune, 2004 ; Kalkun, Andreas. Pääväraamat. Tartu : Erakkond, 2004 ; Jõerüüt, Jaak. Uus raamat. Tallinn : Tuum, 2004 ; Krull, Hasso. Meeter ja Demeeter. Tallinn : Vagabund, 2004 ; Kõiv, Madis. Päev. Tartu : Akkon, 2004 ; Mihkelson, Ene. Uroboros. Tallinn : Tuum, 2004 ; Soomets, Triin. Toormaterjal. Tallinn : Verb, 2004 ; Vaher, Berk. Sekeldaja päevad. Tallinn : Tuum, 2004

VIRTIS-M flight lamps

International Nuclear Information System (INIS)

Melchiorri, R.; Piccioni, G.; Mazzoni, A.

2003-01-01

VIRTIS-M is a visible-infrared (VIS-IR) image spectrometer designed for the Rosetta mission; it intends to provide detailed informations on the physical, chemical, and mineralogical nature of comets and asteroids. The in-flight performances of VIRTIS-M are expected to be influenced by various disturbances, like the initial strong vibrations of the rocket, the long duration of the experiment (from 2003 to 2010), as well as other possible environmental changes; therefore, an in-flight recalibration procedure is mandatory. Quite often in such kinds of missions, a light emission diode (LED) is employed to calibrate the on-board spectrometers by taking advantage of the relative small dimensions, stability, and hardness of these sources. VIRTIS-M is the first image spectrometer that will use a new generation of lamps for internal calibrations. These new lamps are characterized by a wide spectral range with a blackbody-like emission with an effective temperature of about (2400-2600 K), thereby covering the whole VIRTIS-M's spectral range (0.2-5 μm); i.e., they offer the possibility of a wider spectral calibration in comparison with the quasimonochromatic LED emission. A precise spectral calibration is achieved by adding special filters for visible and infrared ranges in front of the window source, containing many narrow absorption lines. In the present article, we describe the calibration and tests of some flight prototypes of these lamps (VIS and IR), realized by the Officine Galileo and calibrated by the Consiglio Nazionale delle Ricerche-Istituto di Astrofisica Spaziale e Fisica Cosmica

Short outlines of books by Estonian authors / Brita Melts, Rutt Hinrikus, Maire Iro and Maret Vaher

Index Scriptorium Estoniae

2013-01-01

Arvustus: Pärtna, Maarja. Läved ja tüved. Tallinn : Eesti Keele Sihtasutus, 2013 ; Sauter, Peeter. Ära jäta mind rahule. Tallinn : P. Sauter, 2012 ; Viiding, Elo. Teised. Tallinn : Tuum, 2012 ; Mathura. Kumalasepäev. Lelle : Allikaäärne, 2012 ; Kadastik, Mart. Kevad saabub sügisel. Tallinn : Varrak, 2013 ; Mutt, Mihkel. Kooparahvas läheb ajalukku. Tallinn : Fabian, 2012 ; Hargla, Indrek. Apteeker Melchior ja Pirita kägistaja. Tallinn : Varrak, 2013 ; Raud, Rein. Rekonstruktsioon. Tallinn : Mustvalge Kirjastus, 2012 ; Toona, Elin. Into exile : a life story of war and peace. Woodsville (N.H.) : Lakeshore Press, 2013 ; Berg, Maimu. Moemaja. Tartu : Petrone Print, 2012 ; Kareva, Doris, Rooste, Jürgen. Elutants. Tallinn : Verb, 2013 ; Ehin, Kristiina. Paleontoloogi päevaraamat. Tartu : Petrone Print, 2013 ; Maria Lee. Stereomeetria. Tallinn : Verb, 2012

The ARGUS time-of-flight system

International Nuclear Information System (INIS)

Heller, R.; Klinger, T.; Salomon, R.; Schubert, K.R.; Stiewe, J.; Waldi, R.; Weseler, S.

1985-01-01

The time-of-flight system of the ARGUS detector at the DORIS e + e - storage ring consists of 64 barrel scintillation counters covering 75% of 4π, and 2x48 end cap counters, covering 17% of 4π. The barrel counters are viewed by two phototubes each, while the end cap counters have one tube only. The time-of-flight system serves as a part of the fast trigger and identifies charged particles. The time resolution achieved during the first year of ARGUS operation is 210 ps for Bhabhas (which are used for the off-line monitoring of the system), and 220 ps for hadrons, both in barrel and end cap counters. This converts into a three standard deviation mass separation up to 700 MeV/c between pions and kaons and 1200 MeV/c between kaons and protons. Electrons can be separated from heavier particles up to 230 MeV/c. (orig.)

Control and Non-Payload Communications (CNPC) Prototype Radio Validation Flight Test Report

Science.gov (United States)

Shalkhauser, Kurt A.; Ishac, Joseph A.; Iannicca, Dennis C.; Bretmersky, Steven C.; Smith, Albert E.

2017-01-01

This report provides an overview and results from the unmanned aircraft (UA) Control and Non-Payload Communications (CNPC) Generation 5 prototype radio validation flight test campaign. The radios used in the test campaign were developed under cooperative agreement NNC11AA01A between the NASA Glenn Research Center and Rockwell Collins, Inc., of Cedar Rapids, Iowa. Measurement results are presented for flight tests over hilly terrain, open water, and urban landscape, utilizing radio sets installed into a NASA aircraft and ground stations. Signal strength and frame loss measurement data are analyzed relative to time and aircraft position, specifically addressing the impact of line-of-sight terrain obstructions on CNPC data flow. Both the radio and flight test system are described.

Lammasinimene, liblikmees ja karunaine : maagilisest realismist eesti kirjanduse näitel / Andrus Org

Index Scriptorium Estoniae

Org, Andrus

2007-01-01

Maagilisest realismist kolme eesti romaani põhjal: Karl Rumori "Krutsifiks" (Tallinn : Eesti Raamat, 1989), Mehis Heinsaare "Härra Pauli kroonikad" (Tallinn : Perioodika, 2001), Nikolai Baturini triloogia "Karu süda" (Tallinn : Eesti Raamat, 1989), "Kartlik Nikas, lõvilakkade kammija" (Tallinn : Eesti Raamat, 1993), "Kentaur" (Tallinn : Eesti Raamat, 2003)

Integrated guidance and control design of a flight vehicle with side-window detection

Directory of Open Access Journals (Sweden)

Tianyu ZHENG

2018-04-01

Full Text Available This paper considers the guidance and control problem of a flight vehicle with side-window detection. In order to guarantee the target remaining in the seeker's sight of view, the line of sight and the attitude of the flight vehicle should be under some constraints caused by the side-window, which leads to coupling between the guidance and the attitude dynamics model. To deal with the side-window constraints and the coupling, a novel Integrated Guidance and Control (IGC design approach is proposed. Firstly, the relative motion equations are derived in the body-Line of Sight (LOS coordinate system. And the guidance and control problem of the flight vehicle is formulated into an IGC problem with state constraints. Then, based on the singular perturbation method, the IGC problem is decomposed into the control design of the quasi-steady-state subsystem and the boundary-layer subsystem which can be designed separately. Finally, the receding horizon control is applied to the control design for the two subsystems. Simulation results show the effectiveness of the proposed approach. Keywords: Integrated guidance and control, Receding horizon control, Side-window detection, Singular perturbation, Terminal guidance

Minimizing the background radiation in the new neutron time-of-flight facility at CERN FLUKA Monte Carlo simulations for the optimization of the n_TOF second experimental line

CERN Document Server

Bergström, Ida; Elfgren, Erik

2013-06-11

At the particle physics laboratory CERN in Geneva, Switzerland, the Neutron Time-of-Flight facility has recently started the construction of a second experimental line. The new neutron beam line will unavoidably induce radiation in both the experimental area and in nearby accessible areas. Computer simulations for the minimization of the background were carried out using the FLUKA Monte Carlo simulation package. The background radiation in the new experimental area needs to be kept to a minimum during measurements. This was studied with focus on the contributions from backscattering in the beam dump. The beam dump was originally designed for shielding the outside area using a block of iron covered in concrete. However, the backscattering was never studied in detail. In this thesis, the fluences (i.e. the flux integrated over time) of neutrons and photons were studied in the experimental area while the beam dump design was modified. An optimized design was obtained by stopping the fast neutrons in a high Z mat...

Lugemis- ja kuulamissoovitusi lapsemeelsetele : [heliraamatud ja -plaadid lastele] / Esme Kassak

Index Scriptorium Estoniae

Kassak, Esme

2010-01-01

Arvustus: Jancis, Kaspar. Seiklus Salamandril, ehk, Morten Viksi uskumatud juhtumised lollide laevas. Tallinn : Menu Kirjastus, 2010 ; Kivirähk, Andrus. Kaka ja kevad [Helisalvestis] / loeb Ülle Kaljuste. Tallinn ; Varrak, 2010 ; Kivirähk, Andrus. Kaelkirjak [Helisalvestis] / loeb Harriet Toompere. Tallinn : Varrak, 2010 ; Tungal, Leelo. Hea lapse laulud [Helisalvestis]. Tallinn : Nõmmelill, 2010 ; Pajusaar, Priit. Lapsed, liblikad ja teised mutukad [Helisalvestis]. Tallinn : Varrak, 2010 ; Toman, Eduard. Gena ja teised : [Helisalvestis]. Tallinn : Greenroom Studio, 2010 ; Vilmusenaho, Marika. Tuulejutu viisid [Helisalvestis] / esitavad Meero Muusiku laululapsed. I.k. : Tempo Rubato, 2009 ; Raud, Eno. Sipsik : laste unejutud / loeb Salme Reek. Tallinn : Eesti Rahvusringhääling, 2010

Miracle Flights

Science.gov (United States)

... a Flight Get Involved Events Shop Miles Contact Miracle Flights Blog Giving Tuesday 800-359-1711 Thousands of children have been saved, but we still have miles to go. Request a Flight Click Here to Donate - Your ...

Arnold Rüütel ja Toomas Hendrik Ilves raamaturiiulil

Index Scriptorium Estoniae

2006-01-01

Arnold Rüütel. Tuleviku taassünd. Tallinn : Ilo, 2001; Toomas Kall. Rüütel : rahva keeles ja meeles. Tallinn : Varrak, 2006; Eesti Vabariigi President Arnold Rüütel. [Tallinn] : Ilo, 2006; Arnold Rüütel. Agraar-tööstuskompleksi areng Eesti NSV-s. Tallinn : Valgus, 1982; Arnold Rüütel. President : [valik Vabariigi Presidendi Arnold Rüütli kõnedest]. Tallinn : Eesti Keele Sihtasutus, 2003; Toomas Hendrik Ilves. Eesti jõudmine. Tallinn : Varrak, 2006

Short outlines of books by Estonian authors / Janika Kronberg and Rutt Hinrikus

Index Scriptorium Estoniae

Kronberg, Janika, 1963-

2010-01-01

Arvustus: Käsper, Kalle. Buridanid. I-V. Tallinn : Eesti Keele Sihtasutus, 2005-2010 ; Kivastik, Mart. Eesti asjad. Tartu : Kaks Musketäri, 2010 ; Kangro, Maarja. Ahvid ja solidaarsus. Tallinn : Eesti keele Sihtasutus, 2010 ; Põder, Rein. Unustatud. Tallinn : Eesti Raamat, 2010 ; Kesküla, Kalev. Elu sumedusest. Tallinn : Tuum, 2009 ; Pilv, Aare. Ramadaan. Tallinn : Tuum, 2010

Mida loed sina? / Indrek Hargla

Index Scriptorium Estoniae

Hargla, Indrek, pseud., 1970-

2007-01-01

Tutvustus: Pérez-Reverte, Arturo. Dumas̀ klubi ehk Richelieu vari. Tallinn : Varrak, 2006 ; Belials, Veiko. Jumalate vandenõu. Tallinn : Varrak, 2006 ; Põder, Rein. Eike. Tallinn : Eesti Raamat, 2006 ; Reeve, Philip. Kuldseeklid. Tallinn : Tiritamm, 2006 ; Martin, George R. R. Troonide mäng. Esimene raamat / tlk. Mario Kivistik. Tallinn : Varrak, 2006. (Jää ja tule laul) (F-sari)

HOPE: An On-Line Piloted Handling Qualities Experiment Data Book

Science.gov (United States)

Jackson, E. B.; Proffitt, Melissa S.

2010-01-01

A novel on-line database for capturing most of the information obtained during piloted handling qualities experiments (either flight or simulated) is described. The Hyperlinked Overview of Piloted Evaluations (HOPE) web application is based on an open-source object-oriented Web-based front end (Ruby-on-Rails) that can be used with a variety of back-end relational database engines. The hyperlinked, on-line data book approach allows an easily-traversed way of looking at a variety of collected data, including pilot ratings, pilot information, vehicle and configuration characteristics, test maneuvers, and individual flight test cards and repeat runs. It allows for on-line retrieval of pilot comments, both audio and transcribed, as well as time history data retrieval and video playback. Pilot questionnaires are recorded as are pilot biographies. Simple statistics are calculated for each selected group of pilot ratings, allowing multiple ways to aggregate the data set (by pilot, by task, or by vehicle configuration, for example). Any number of per-run or per-task metrics can be captured in the database. The entire run metrics dataset can be downloaded in comma-separated text for further analysis off-line. It is expected that this tool will be made available upon request

Short outlines of books by Estonian authors / Leena Kurvet-Käosaar, Brita Melts, Rutt Hinrikus and Janika Kronberg

Index Scriptorium Estoniae

2011-01-01

Arvustus: Nurklik, Siim. Kas ma olen nüüd elus. Tallinn : S. Nurklik, 2010 ; Lintrop, Aado. Annapurna. Tartu : Ilmamaa, 2010 ; Lintrop, Aado. Õhtud sõidavad õue. Tartu : Ilmamaa, 2011 ; Saar, Anti. Tekste siledast ruumist. Tallinn : Eesti Keele Sihtasutus, 2009 ; Hvostov, Andrei. Sillamäe passioon. Tartu : Petrone Print, 2011 ; Nõu, Helga. Valetaja. Tallinn : Eesti Ajalehed, 2011 ; Malin, Jaan. Alati vahe. Tallinn : Tuum, 2010 ; Jõerüüt, Jaak. Muutlik. Tallinn : Tuum, 2010 ; Luik, Viivi. Varjuteater. Tallinn : Eesti Keele Sihtasutus, 2010

Short outlines of books by Estonian authors / Brita Melts, Rutt Hinrikus and Janika Kronberg

Index Scriptorium Estoniae

Melts, Brita

2012-01-01

Arvustus: Kilusk, Ott. Veidrikud ja võpatused. Tallinn : Menu, 2012 ; Kilusk, Ott. Oktoobrikuine tuuker. Tallinn : Kirjastuskeskus, 2010 ; Hansen, Aime. Ma olin mereingel. Tallinn : Verb, 2011 ; Vallisoo, Mari. Koidutäht koolivihikus. Tartu : Ilmamaa, 2011 ; Sinijärv, Karl Martin. Krümitor 0671. Tallinn ; Näo Kirik, 2011 ; Aareleid, Kai. Vene veri. Tallinn : Varrak, 2011 ; Ashilevi, Jim. Ma olen elus olemise tunne. Luige : Verb, 2011 ; Traat, Mats. Vastsed Harala elulood. Tartu : Ilmamaa, 2011 ; Tamm, Margus. Unesnõiduja. Tallinn : Raudwara, 2011

Laboratory measurements of the x-ray line emission from neon-like Fe XVII

International Nuclear Information System (INIS)

Brown, G V; Beiersdorfer, P; Chen, H; Scofield, J; Boyce, K R; Kelley, R L; Kilbourne, C A; Porter, F S; Gu, M F; Kahn, S M; Szymkowiak, A E

2006-01-01

The authors have conducted a systematic study of the dominant x-ray line emission from Fe XVII. These studies include relative line intensities in the optically thin limit, intensities in the presence of radiation from satellite lines from lower charge states of iron, and the absolute excitation cross sections of some of the strongest lines. These measurements were conducted at the Lawrence Livermore National Laboratory electron beam ion trap facility using crystal spectrometers and a NASA-Goddard Space Flight Center microcalorimeter array

Short outlines of books by Estonian authors / Janika Kronberg, Rutt Hinrikus

Index Scriptorium Estoniae

Kronberg, Janika, 1963-

2003-01-01

Sinijärv, Karl- Martin. Artutart & 39. Tallinn : Tuum, 2002 ; Beier, Priidu. Monaco. Tartu : P. Beier, 2002 ; Malin, Jaan. Sulle. Tartu : J. Malin, 2003 ; Liiv, Toomas. Luuletused 1968-2002. Tallinn : Tuum, 2003 ; Mägi, Arvo. Katk ja koolera. Tartu : Ilmamaa ; Kross, Jaan. Omaeluloolisus ja alltekst. Tallinn : Eesti Keele Sihtasutus, 2003 ; Kaplinski, Jaan ; Salminen, Johannes. Ööd valged ja mustad. Tallinn : Loomingu Raamatukogu, 2003 ; Kauksi Ülle. Käänüpäiv. Tartu : Kauksi Ülle Mänedsment', 2003 ; Luik, Tõnu. Filosoofiast kõnelda. Tartu : Ilmamaa, 2002 ; Teder, Tarmo. Pööningujutud. Tallinn : Eesti Keele Sihtasutus, 2002 ; Vetemaa, Enn. Minu väga magus elu ehk martsipanimeister. Tallinn : Tänapäev, 2002 ; Põldroos, Enn. Joonik kivi. Tallinn : Eesti Keele Sihtasutus, 2003 ; Suburg, Lilli. Kogutud kirjatööd. Tallinn : Eesti Raamat, 2002 ; Mikelsaar, Henn. Müüritud. Tartu : Ilmamaa, 2003 ; Kaus, Jan. Õndsate tund. Tallinn : Tuum, c2003

Book reviews / by Jürgen Rooste and Paul Raud

Index Scriptorium Estoniae

Rooste, Jürgen, 1979-

2016-01-01

Arvustus: Sinijärv, Karl Martin. KMSX: kuidas öelda. Tallinn Näo Kirik, 2016 ; Heinsaar, Mehis. Unistuste tappev kasvamine. Tallinn : Menu, 2016 ; Friedenthal, Meelis. Inglite keel. Tallinn : Varrak, 2016 ; Filimonov, P. I. Laulis, kuni kõik lõppes / tõlkinud Ingrid Velbaum-Staub. Tallinn : Varrak, 2016 ; Urgas, Silvia. Siht/Koht. Tartu : Elusamus, 2015 ; Kaus, Jan. Läheduste raamat. Tallinn : Verb, 2016

Emergency Flight Control of a Twin-Jet Commercial Aircraft using Manual Throttle Manipulation

Science.gov (United States)

Cole, Jennifer H.; Cogan, Bruce R.; Fullerton, C. Gordon; Burken, John J.; Venti, Michael W.; Burcham, Frank W.

2007-01-01

a survivable runway landing using TOC. The PCAR project objective was a set of pilot procedures for operation of a specific aircraft without hydraulics that (a) have been validated in both simulation and flight by relevant personnel, and (b) mesh well with existing commercial operations, maintenance, and training at a minimum cost. As a result of this study, a procedure has been developed to assist a crew in making a survivable landing using TOC. In a simulation environment, line pilots with little or no previous TOC experience performed survivable runway landings after a few practice TOC approaches. In-flight evaluations put line pilots in a simulated emergency situation where TOC was used to recover the aircraft, maneuver to a landing site, and perform an approach down to 200 feet AGL. The results of this research, including pilot observations, procedure comments, recommendations, future work and lessons learned, will he discussed. Flight data and video footage of TOC approaches may also be shown.

Kolm kogumikku Eesti ajaloolisi linnaplaane / Heino Mardiste

Index Scriptorium Estoniae

Mardiste, Heino, 1936-

2016-01-01

Tutvustus: Eesti linnade plaanid 1584-2011 [Kaart] / koostaja Tõnu Raid. Tallinn : Grenader, 2013 ; Tartu ajaloolistel linnaplaanidel 1600-2010 [Kaart] / koostaja Tõnu Raid. Tallinn : Grenader, 2015 ; Tallinn ajaloolistel linnaplaanidel 1634-1989 [Kaart] / koostaja Tõnu Raid. Tallinn : Grenader, 2011

First on-line applications of multi-reflection time-of-flight mass separator at ISOLTRAP and the mass measurement of $^{82}$Zn

CERN Document Server

Wolf, Robert

This thesis describes the implementation and first on-line application of a multi-reflection time-of-flight (MR-ToF) mass analyzer for high-resolution mass separation at the ISOLTRAP mass spectrometer at ISOLDE/CERN. On the one hand, the major objective was to improve ISOLTRAPs mass-measurement capabilities with respect to the ratio of delivered contaminating ions to ions of interest. On the other hand, the time necessary to purify wanted from unwanted species should be reduced as much as possible to enable access to even more exotic nuclei. The device has been set up, optimized and tested at the University of Greifswald before its move to ISOLTRAP. The achieved performance comprises mass resolving powers of up to 200000 reached at observation times of 30ms and a contamination suppression of about four orders of magnitude by use of a Bradbury-Nielsen gate. With the characteristics, it outperforms clearly the so far state-of-the-art purification method of a gas-filled Penning trap. To improve the utilization o...

Analysis of Return and Forward Links from STARS' Flight Demonstration 1

Science.gov (United States)

Gering, James A.

2003-01-01

Space-based Telemetry And Range Safety (STARS) is a Kennedy Space Center (KSC) led proof-of-concept demonstration, which utilizes NASA's space network of Tracking and Data Relay Satellites (TDRS) as a pathway for launch and mission related information streams. Flight Demonstration 1 concluded on July 15,2003 with the seventh flight of a Low Power Transmitter (LPT) a Command and Data Handler (C&DH), a twelve channel GPS receiver and associated power supplies and amplifiers. The equipment flew on NASA's F-I5 aircraft at the Dryden Flight Research Center located at Edwards Air Force Base in California. During this NASA-ASEE Faculty Fellowship, the author participated in the collection and analysis of data from the seven flights comprising Flight Demonstration 1. Specifically, the author examined the forward and return links bit energy E(sub B) (in Watt-seconds) divided by the ambient radio frequency noise N(sub 0) (in Watts / Hertz). E(sub b)/N(sub 0) is commonly thought of as a signal-to-noise parameter, which characterizes a particular received radio frequency (RF) link. Outputs from the data analysis include the construction of time lines for all flights, production of graphs of range safety values for all seven flights, histograms of range safety E(sub b)/N(sub 0) values in five dB increments, calculation of associated averages and standard deviations, production of graphs of range user E(sub b)/N(sub 0) values for the all flights, production of graphs of AGC's and E(sub b)/N(sub 0) estimates for flight 1, recorded onboard, transmitted directly to the launch head and transmitted through TDRS. The data and graphs are being used to draw conclusions related to a lower than expected signal strength seen in the range safety return link.

IXV re-entry demonstrator: Mission overview, system challenges and flight reward

Science.gov (United States)

Angelini, Roberto; Denaro, Angelo

2016-07-01

The Intermediate eXperimental Vehicle (IXV) is an advanced re-entry demonstrator vehicle aimed to perform in-flight experimentation of atmospheric re-entry enabling systems and technologies. The IXV integrates key technologies at the system level, with significant advancements on Europe's previous flying test-beds. The project builds on previous achievements at system and technology levels, and provides a unique and concrete way of establishing and consolidating Europe's autonomous position in the strategic field of atmospheric re-entry. The IXV mission and system objectives are the design, development, manufacturing, assembling and on-ground to in-flight verification of an autonomous European lifting and aerodynamically controlled reentry system, integrating critical re-entry technologies at system level. Among such critical technologies of interest, special attention is paid to aerodynamic and aerothermodynamics experimentation, including advanced instrumentation for aerothermodynamics phenomena investigations, thermal protections and hot-structures, guidance, navigation and flight control through combined jets and aerodynamic surfaces (i.e. flaps), in particular focusing on the technologies integration at system level for flight. Following the extensive detailed design, manufacturing, qualification, integration and testing of the flight segment and ground segment elements, IXV has performed a full successful flight on February 11th 2015. After the launch with the VEGA launcher form the CSG spaceport in French Guyana, IXV has performed a full nominal mission ending with a successful splashdown in the Pacific Ocean. During Flight Phase, the IXV space and ground segments worked perfectly, implementing the whole flight program in line with the commanded maneuvers and trajectory prediction, performing an overall flight of 34.400 km including 7.600 km with hot atmospheric re-entry in automatic guidance, concluding with successful precision landing at a distance of ~1

Short outlines of books by Estonian authors / Janika Kronberg, Rutt Hinrikus

Index Scriptorium Estoniae

Kronberg, Janika, 1963-

2005-01-01

Tutvustus: Henno, Sass. Mina olin siin. 1 : esimene arest. Tallinn : Eesti Päevaleht, 2005 ; Kruusvall, Jaan. Sinetavad kaugused : valitud proosat. Tallinn : Eesti Raamat, 2004 ; Hirv, Indrek. Klaaskübara all : [esseed]. Tartu : Ilmamaa, 2004 ; Õudne Eesti : valimik eesti õudusjutte. Tallinn : Varrak, 2005 ; Ruitlane, Olavi. Kroonu. Räpina : Väiku Välläandja, 2005 ; Ehin, Kristiina. Kaitseala. Tallinn : Huma, 2005 ; Kivirähk, Andrus. Jutud. Tallinn : Eesti Kirjanduse Sihtasutus, 2005 ; Talvet, Jüri. Unest, lumest. Tartu : Ilmamaa, 2005 ; Künnap, Asko. Kõige ilusam sõda. Tallinn : Näo Kirik, 2004 ; Kaplinski, Jaan. Kaks päikest : teistmoodi muinaslood. Tallinn : Tänapäev, 2005 ; Alver, Betti. Koguja : suur luuleraamat. Tartu : Ilmamaa, 2005

Short outlines of books by Estonian authors / Brita Melts, Rutt Hinrikus and Janika Kronberg

Index Scriptorium Estoniae

Melts, Brita

2015-01-01

Arvustus: Viitol, Livia. Jutte ja novelle. Tallinn : Libri Livoniae, 2014 ; Talvet, Jüri. Ten Letters to Montaigne : "Self" and "other". Tartu : Tartu Ülikooli Kirjastus, 2014 ; Rooste, Jürgen. Suur sume, suur tume. [Luige (Kiili vald)] : Verb, 2014 ; Kross, Märten. Hullumäng. [Tallinn] : Tammerraamat, 2014 ; Kaus, Jan. Ma olen elus. Tallinn : Tuum, 2014 ; Kangro, Maarja. Hüppa tulle. Tallinn : Nähtamatu Ahv, 2014 ; Kasemaa, Andrus. Minu viimane raamat. Tallinn : Varrak, 2014 ; Raik, Katri. Minu Narva : kahe maailma vahel. [Tartu] : Petrone Print, 2013 ; Kareva, Doris. Maailma asemel. [Kordustr. Tallinn] : Verb, 2014

Nobelistid : süütuse rebestus ja üllatus / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

2008-01-01

Tutvustatakse 2008. a. eesti keeles ilmunud Nobeli kirjandusauhinna laureaatide jt. teoseid: Faulkner, William. Absalom, Absalom! / tlk. Kersti Unt. Tallinn : Tänapäev, 2008 ; Dostojevski, Fjodor. Alandatud ja solvatud / tlk. Leopold Kenn. Tallinn : Eesti Raamat, 2008 ; Böll, Heinrich. Ametisõidu lõpp / tlk. Mati Sirkel. Tallinn : Varrak, 2008 ; Morrison, Toni. Dzhäss / tlk. Udo Uibo ja Krista Kaer. Tallinn : Varrak, 2008 ; Laxness, Halld̤r. Islandi kell / tlk. Arvo Alas ja Askur Alas. Tallinn : Varrak, 2008 ; Bunin, Ivan. Armastuse grammatika : [novellid] / koost. Rein Põder ; tlk. Jüri Pärni. Tallinn : Eesti Raamat, 2008

Contribution of time-of-flight information to limited-angle positron tomography

International Nuclear Information System (INIS)

Macdonald, B.; Perez-Mendez, V.; Tam, K.C.

1981-10-01

Limited-angle emission tomography was investigated using a two-dimensional phantom to generate positron events simulating a camera with two opposed parallel position-sensitive detectors collecting data within a 90 0 cone. The data, backprojected onto lines passing through the phantom volume, is used with a matrix reconstruction method to provide two-dimensional images. Image quality was measured using the standard deviation of the reconstructions with respect to the original phantom. The application of Phillips-Twomey smoothing to the deconvolution matrices has substantially improved the original reconstructions, a factor of 1.9 in signal to noise ratio, giving S/N = 3.4 for a phantom having an average of 150 events/pixel. Using photon time-of-flight to restrict the reconstruction volume a further considerable improvement is made. When the time-of-flight limited the contributing volume to 4 lines out of 11 the improvement was another factor of 1.9 giving S/N = 6.0 for the same phantom. Comparable increases in signal to noise ratios are expected for three-dimensional reconstructions

Time coder for slow neutron time-of-flight spectrometer

International Nuclear Information System (INIS)

Grashilin, V.A.; Ofengenden, R.G.

1988-01-01

Time coder for slow neutron time-of-flight spectrometer is described. The time coder is of modular structure, is performed in the CAMAC standard and operates on line with DVK-2 computer. The main coder units include supporting generator, timers, time-to-digital converter, memory unit and crate controller. Method for measuring background symmetrically to the effect is proposed for a more correct background accounting. 4 refs.; 1 fig

AirSTAR Hardware and Software Design for Beyond Visual Range Flight Research

Science.gov (United States)

Laughter, Sean; Cox, David

2016-01-01

The National Aeronautics and Space Administration (NASA) Airborne Subscale Transport Aircraft Research (AirSTAR) Unmanned Aerial System (UAS) is a facility developed to study the flight dynamics of vehicles in emergency conditions, in support of aviation safety research. The system was upgraded to have its operational range significantly expanded, going beyond the line of sight of a ground-based pilot. A redesign of the airborne flight hardware was undertaken, as well as significant changes to the software base, in order to provide appropriate autonomous behavior in response to a number of potential failures and hazards. Ground hardware and system monitors were also upgraded to include redundant communication links, including ADS-B based position displays and an independent flight termination system. The design included both custom and commercially available avionics, combined to allow flexibility in flight experiment design while still benefiting from tested configurations in reversionary flight modes. A similar hierarchy was employed in the software architecture, to allow research codes to be tested, with a fallback to more thoroughly validated flight controls. As a remotely piloted facility, ground systems were also developed to ensure the flight modes and system state were communicated to ground operations personnel in real-time. Presented in this paper is a general overview of the concept of operations for beyond visual range flight, and a detailed review of the airborne hardware and software design. This discussion is held in the context of the safety and procedural requirements that drove many of the design decisions for the AirSTAR UAS Beyond Visual Range capability.

Flight Test Implementation of a Second Generation Intelligent Flight Control System

Science.gov (United States)

Williams-Hayes, Peggy S.

2005-01-01

The NASA F-15 Intelligent Flight Control System project team has developed a series of flight control concepts designed to demonstrate the benefits of a neural network-based adaptive controller. The objective of the team was to develop and flight-test control systems that use neural network technology, to optimize the performance of the aircraft under nominal conditions, and to stabilize the aircraft under failure conditions. Failure conditions include locked or failed control surfaces as well as unforeseen damage that might occur to the aircraft in flight. The Intelligent Flight Control System team is currently in the process of implementing a second generation control scheme, collectively known as Generation 2 or Gen 2, for flight testing on the NASA F-15 aircraft. This report describes the Gen 2 system as implemented by the team for flight test evaluation. Simulation results are shown which describe the experiment to be performed in flight and highlight the ways in which the Gen 2 system meets the defined objectives.

Journey towards yourself / Rein Veidemann

Index Scriptorium Estoniae

Veidemann, Rein, 1946-

2011-01-01

Arvustus: Luik, Viivi. Varjuteater. Tallinn : Eesti Keele Sihtasutus, 2010 ; Luik, Viivi, Rosma, Hedi. Ma olen raamat. Tallinn : SE & JS, 2010 ; Jõerüüt, Jaak. Armastuse laiad, kõrged hooned. Tallinn : Tuum, 2010 ; Jõerüüt, Jaak. Muutlik. Tallinn : Tuum, 2010

Evidence of Decay of Flux Ratio of Fe to Fe–Ni Line Features with ...

Indian Academy of Sciences (India)

2010-08-18

Aug 18, 2010 ... measuring of the intensity and mean energy of the Fe and Fe–Ni line ... The instrumentation of the SLD payload, its in-flight calibration and operation ... reconnection process and also decays faster compared to many other ... measure vary over time and these factors mainly control the shape of the line. The.

Model–Based Techniques for Virtual Sensing of Longitudinal Flight Parameters

Directory of Open Access Journals (Sweden)

Seren Cédric

2015-03-01

Full Text Available Introduction of fly-by-wire and increasing levels of automation significantly improve the safety of civil aircraft, and result in advanced capabilities for detecting, protecting and optimizing A/C guidance and control. However, this higher complexity requires the availability of some key flight parameters to be extended. Hence, the monitoring and consolidation of those signals is a significant issue, usually achieved via many functionally redundant sensors to extend the way those parameters are measured. This solution penalizes the overall system performance in terms of weight, maintenance, and so on. Other alternatives rely on signal processing or model-based techniques that make a global use of all or part of the sensor data available, supplemented by a model-based simulation of the flight mechanics. That processing achieves real-time estimates of the critical parameters and yields dissimilar signals. Filtered and consolidated information is delivered in unfaulty conditions by estimating an extended state vector, including wind components, and can replace failed signals in degraded conditions. Accordingly, this paper describes two model-based approaches allowing the longitudinal flight parameters of a civil A/C to be estimated on-line. Results are displayed to evaluate the performances in different simulated and real flight conditions, including realistic external disturbances and modeling errors.

Neli vaadet tuumale ja näivusele / Märt Väljataga

Index Scriptorium Estoniae

Väljataga, Märt, 1965-

2009-01-01

Arvustus: Tuglas, Friedebert. Valik proosat / koostanud ja saatetekstid kirjutanud Jaan Undusk. Tallinn : Avita, 2009 ; Nietzsche, Friedrich. Tragöödia sünd. Tallinn : Tänapäev, 2009 ; Kesküla, Kalev. Elu sumedusest. Tallinn : Tuum, 2009 ; Sirkel, Mati. Uued orva-aastad. Kommentaarium. Tallinn : Tuum, 2009

Supporting Development of Satellite's Guidance Navigation and Control Software: A Product Line Approach

Science.gov (United States)

McComas, David; Stark, Michael; Leake, Stephen; White, Michael; Morisio, Maurizio; Travassos, Guilherme H.; Powers, Edward I. (Technical Monitor)

2000-01-01

The NASA Goddard Space Flight Center Flight Software Branch (FSB) is developing a Guidance, Navigation, and Control (GNC) Flight Software (FSW) product line. The demand for increasingly more complex flight software in less time while maintaining the same level of quality has motivated us to look for better FSW development strategies. The GNC FSW product line has been planned to address the core GNC FSW functionality very similar on many recent low/near Earth missions in the last ten years. Unfortunately these missions have not accomplished significant drops in development cost since a systematic approach towards reuse has not been adopted. In addition, new demands are continually being placed upon the FSW which means the FSB must become more adept at providing GNC FSW functionality's core so it can accommodate additional requirements. These domain features together with engineering concepts are influencing the specification, description and evaluation of FSW product line. Domain engineering is the foundation for emerging product line software development approaches. A product line is 'A family of products designed to take advantage of their common aspects and predicted variabilities'. In our product line approach, domain engineering includes the engineering activities needed to produce reusable artifacts for a domain. Application engineering refers to developing an application in the domain starting from reusable artifacts. The focus of this paper is regarding the software process, lessons learned and on how the GNC FSW product line manages variability. Existing domain engineering approaches do not enforce any specific notation for domain analysis or commonality and variability analysis. Usually, natural language text is the preferred tool. The advantage is the flexibility and adapt ability of natural language. However, one has to be ready to accept also its well-known drawbacks, such as ambiguity, inconsistency, and contradictions. While most domain analysis

Method and system for control of upstream flowfields of vehicle in supersonic or hypersonic atmospheric flight

Science.gov (United States)

Daso, Endwell O. (Inventor); Pritchett, II, Victor E. (Inventor); Wang, Ten-See (Inventor); Farr, Rebecca Ann (Inventor)

2012-01-01

The upstream flowfield of a vehicle traveling in supersonic or hypersonic atmospheric flight is actively controlled using attribute(s) experienced by the vehicle. Sensed attribute(s) include pressure along the vehicle's outer mold line, temperature along the vehicle's outer mold line, heat flux along the vehicle's outer mold line, and/or local acceleration response of the vehicle. A non-heated, non-plasma-producing gas is injected into an upstream flowfield of the vehicle from at least one surface location along the vehicle's outer mold line. The pressure of the gas so-injected is adjusted based on the attribute(s) so-sensed.

A Survey of Open-Source UAV Flight Controllers and Flight Simulators

DEFF Research Database (Denmark)

Ebeid, Emad Samuel Malki; Skriver, Martin; Terkildsen, Kristian Husum

2018-01-01

, which are all tightly linked to the UAV flight controller hardware and software. The lack of standardization of flight controller architectures and the use of proprietary closed-source flight controllers on many UAV platforms, however, complicates this work: solutions developed for one flight controller...... may be difficult to port to another without substantial extra development and testing. Using open-source flight controllers mitigates some of these challenges and enables other researchers to validate and build upon existing research. This paper presents a survey of the publicly available open...

The role of situation assessment and flight experience in pilots' decisions to continue visual flight rules flight into adverse weather.

Science.gov (United States)

Wiegmann, Douglas A; Goh, Juliana; O'Hare, David

2002-01-01

Visual flight rules (VFR) flight into instrument meteorological conditions (IMC) is a major safety hazard in general aviation. In this study we examined pilots' decisions to continue or divert from a VFR flight into IMC during a dynamic simulation of a cross-country flight. Pilots encountered IMC either early or later into the flight, and the amount of time and distance pilots flew into the adverse weather prior to diverting was recorded. Results revealed that pilots who encountered the deteriorating weather earlier in the flight flew longer into the weather prior to diverting and had more optimistic estimates of weather conditions than did pilots who encountered the deteriorating weather later in the flight. Both the time and distance traveled into the weather prior to diverting were negatively correlated with pilots' previous flight experience. These findings suggest that VFR flight into IMC may be attributable, at least in part, to poor situation assessment and experience rather than to motivational judgment that induces risk-taking behavior as more time and effort are invested in a flight. Actual or potential applications of this research include the design of interventions that focus on improving weather evaluation skills in addition to addressing risk-taking attitudes.

Kerge kohmetus soomeugri veere naisteväe keskel / Lauri Sommer

Index Scriptorium Estoniae

Sommer, Lauri, 1973-

2003-01-01

Arvustus: Neli komilannat / tõlkinud Leelo Tungal ja Arvo Valton. Tallinn : Virgela, 1998 ; Neli marilannat / tõlkinud Leelo Tungal. Tallinn : Virgela, 1998 ; Neli mordvalannat / tõlkinud Peeter Volkonski ja Arvo Valton. Tallinn : Virgela, 1998 ; Neli udmurditari / tõlkinud Ellen Niit, Valeeria Villandi ja Arvo Valton. Tallinn : Virgela, 2002

Äratundmisi soome-ugri naisluulet lugedes / Veronika Kivisilla

Index Scriptorium Estoniae

Kivisilla, Veronika

2003-01-01

Arvustus: Neli komilannat / tõlkinud Leelo Tungal ja Arvo Valton. Tallinn : Virgela, 1998 ; Neli marilannat / tõlkija Leelo Tungal. Tallinn : Virgela, 1998 ; Neli mordvalannat / tõlkinud Peeter Volkonski ja Arvo Valton. Tallinn : Virgela, 1998 ; Neli udmurditari / tõlkinud Ellen Niit, Valeeria Villandi ja Arvo Valton. Tallinn : Virgela, 2002

Kohanenud kirjandus : tänase kirjaniku - ja ka tema lugeja elu sisu määravad majanduslikud argumendid, mitte moraalsed valikud / Kärt Hellerma

Index Scriptorium Estoniae

Hellerma, Kärt, 1956-

2005-01-01

Arvustus: Delerm, Philippe. Väikesed naudingud. Tallinn : Varrak, 2004 ; Nothomb, Amélie. Jumala lapsepõlv. Tallinn : Varrak, 2004 ; Darrieussecq, Marie. Minu beebi. Tallinn : Varrak, 2005. Ilmunud ka kogumikus: Hellerma, Kärt. Kohanenud kirjandus : valik kirjanduskriitikat 1987-2006. Eesti Keele Sihtasutus : Tallinn, 2006. Lk. 189-195, pealk. Kohanenud kirjandus

Theseus in Flight

Science.gov (United States)

1996-01-01

The twin pusher propeller-driven engines of the Theseus research aircraft can be clearly seen in this photo, taken during a 1996 research flight at NASA's Dryden Flight Research Center, Edwards, California. The Theseus aircraft, built and operated by Aurora Flight Sciences Corporation, Manassas, Virginia, was a unique aircraft flown at NASA's Dryden Flight Research Center, Edwards, California, under a cooperative agreement between NASA and Aurora. Dryden hosted the Theseus program, providing hangar space and range safety for flight testing. Aurora Flight Sciences was responsible for the actual flight testing, vehicle flight safety, and operation of the aircraft. The Theseus remotely piloted aircraft flew its maiden flight on May 24, 1996, at Dryden. During its sixth flight on November 12, 1996, Theseus experienced an in-flight structural failure that resulted in the loss of the aircraft. As of the beginning of the year 2000, Aurora had not rebuilt the aircraft. Theseus was built for NASA under an innovative, $4.9 million fixed-price contract by Aurora Flight Sciences Corporation and its partners, West Virginia University, Morgantown, West Virginia, and Fairmont State College, Fairmont, West Virginia. The twin-engine, unpiloted vehicle had a 140-foot wingspan, and was constructed largely of composite materials. Powered by two 80-horsepower, turbocharged piston engines that drove twin 9-foot-diameter propellers, Theseus was designed to fly autonomously at high altitudes, with takeoff and landing under the active control of a ground-based pilot in a ground control station 'cockpit.' With the potential ability to carry 700 pounds of science instruments to altitudes above 60,000 feet for durations of greater than 24 hours, Theseus was intended to support research in areas such as stratospheric ozone depletion and the atmospheric effects of future high-speed civil transport aircraft engines. Instruments carried aboard Theseus also would be able to validate satellite

A Simple Flight Mill for the Study of Tethered Flight in Insects.

Science.gov (United States)

Attisano, Alfredo; Murphy, James T; Vickers, Andrew; Moore, Patricia J

2015-12-10

Flight in insects can be long-range migratory flights, intermediate-range dispersal flights, or short-range host-seeking flights. Previous studies have shown that flight mills are valuable tools for the experimental study of insect flight behavior, allowing researchers to examine how factors such as age, host plants, or population source can influence an insects' propensity to disperse. Flight mills allow researchers to measure components of flight such as speed and distance flown. Lack of detailed information about how to build such a device can make their construction appear to be prohibitively complex. We present a simple and relatively inexpensive flight mill for the study of tethered flight in insects. Experimental insects can be tethered with non-toxic adhesives and revolve around an axis by means of a very low friction magnetic bearing. The mill is designed for the study of flight in controlled conditions as it can be used inside an incubator or environmental chamber. The strongest points are the very simple electronic circuitry, the design that allows sixteen insects to fly simultaneously allowing the collection and analysis of a large number of samples in a short time and the potential to use the device in a very limited workspace. This design is extremely flexible, and we have adjusted the mill to accommodate different species of insects of various sizes.

X-1A in flight with flight data superimposed

Science.gov (United States)

1953-01-01

This photo of the X-1A includes graphs of the flight data from Maj. Charles E. Yeager's Mach 2.44 flight on December 12, 1953. (This was only a few days short of the 50th anniversary of the Wright brothers' first powered flight.) After reaching Mach 2.44, then the highest speed ever reached by a piloted aircraft, the X-1A tumbled completely out of control. The motions were so violent that Yeager cracked the plastic canopy with his helmet. He finally recovered from a inverted spin and landed on Rogers Dry Lakebed. Among the data shown are Mach number and altitude (the two top graphs). The speed and altitude changes due to the tumble are visible as jagged lines. The third graph from the bottom shows the G-forces on the airplane. During the tumble, these twice reached 8 Gs or 8 times the normal pull of gravity at sea level. (At these G forces, a 200-pound human would, in effect, weigh 1,600 pounds if a scale were placed under him in the direction of the force vector.) Producing these graphs was a slow, difficult process. The raw data from on-board instrumentation recorded on oscillograph film. Human computers then reduced the data and recorded it on data sheets, correcting for such factors as temperature and instrument errors. They used adding machines or slide rules for their calculations, pocket calculators being 20 years in the future. Three second generation Bell Aircraft Corporations X-1s were built, though four were requested. They were the X-1A (48-1384); X-1B (48-1385); X-1C (canceled and never built); X-1D (48-1386). These aircraft were similar to the X-1s, except they were five feet longer, had conventional canopies, and were powered by Reaction Motors, Inc. XLR11-RM-5 rocket engines. The RM-5, like the previous engines, had no throttle and was controlled by igniting one or more of the four thrust chambers at will. The original program outline called for the X-1A and X-1B to be used for dynamic stability and air loads investigations. The X-1D was to be used

Kägiseva lindi lood : kassetiaegne unustatud muss / Dr Alimentado

Index Scriptorium Estoniae

Dr Alimentado

2009-01-01

1980-ndate lõpul ja 1990-ndate algul väljaantud helikassettidest: Lost Kolchoses. Kainestusmajas. I.k., i.a. ; B.D.Ö. Anblögged. Tallinn : B.D.Ö., 1993 ; Röövel Ööbik. Ilu. Tallinn : Kuldnokk, 1989 ; Rock the Christmas / Velikije Luki, Röövel Ööbik, Kumikameli ... [jt.]. Tallinn : Kuldnokk, i.a. ; Merry Christmas Mr. Lawrence. Graffity revolution. Tallinn : Kuldnokk, i.a. ; J.M.K.E. Rumal nali. Tallinn : Fucking Cunts Records, 1996

Flight Simulation of ARES in the Mars Environment

Science.gov (United States)

Kenney, P. Sean; Croom, Mark A.

2011-01-01

A report discusses using the Aerial Regional- scale Environmental Survey (ARES) light airplane as an observation platform on Mars in order to gather data. It would have to survive insertion into the atmosphere, fly long enough to meet science objectives, and provide a stable platform. The feasibility of such a platform was tested using the Langley Standard Real- Time Simulation in C++. The unique features of LaSRS++ are: full, six-degrees- of-freedom flight simulation that can be used to evaluate the performance of the aircraft in the Martian environment; capability of flight analysis from start to finish; support of Monte Carlo analysis of aircraft performance; and accepting initial conditions from POST results for the entry and deployment of the entry body. Starting with a general aviation model, the design was tweaked to maintain a stable aircraft under expected Martian conditions. Outer mold lines were adjusted based on experience with the Martian atmosphere. Flight control was modified from a vertical acceleration control law to an angle-of-attack control law. Navigation was modified from a vertical acceleration control system to an alpha control system. In general, a pattern of starting with simple models with well-understood behaviors was selected and modified during testing.

Time-dependent scattering in resonance lines

International Nuclear Information System (INIS)

Kunasz, P.B.

1983-01-01

A numerical finite-difference method is presented for the problem of time-dependent line transfer in a finite slab in which material density is sufficiently low that the time of flight between scatterings greatly exceeds the relaxation time of the upper state of the scattering transition. The medium is assumed to scatter photons isotropically, with complete frequency redistribution. Numerical solutions are presented for a homogeneous, time-independent slab illuminated by an externally imposed radiation field which enters the slab at t = 0. Graphical results illustrate relaxation to steady state of trapped internal radiation, emergent energy, and emergent profiles. A review of the literature is also given in which the time-dependent line transfer problem is discussed in the context of recent analytical work

Reis Rosenbergi ajudesse / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

2007-01-01

Lugemismuljeid raamatutest: Piper, Ernst. Alfred Rosenberg : Hitleri peaideoloog. Tallinn : Tänapäev, 2007 ; Judt, Tony. Pärast sõda. Euroopa ajalugu 1945. aastast. Tallinn : Varrak, 2007 ; Döblin, Alfred. Berliin, Alexanderplatz / tlk. Mati Sirkel. Tallinn : Tänapäev, 2007 ; Adson, Artur. Siuru-raamat. Tallinn : Tänapäev, 2007

Neetud Siber / Mihkel Mutt

Index Scriptorium Estoniae

Mutt, Mihkel, 1953-

2004-01-01

Rets. rmt.: Brzezinski, Zbigniew. Suur malelaud. Tallinn, 2003 ; Sergejev, Vladimir ; Vseviov, David. Venemaa - lähedane ja kauge. Tallinn, 2002 ; Figes, Orlando. Natasha tants. Venemaa kultuurilugu. Tallinn, 2003 ; Lotman, Juri. Vestlusi vene kultuurist. Vene aadli argielu ja traditsioonid 18. sajandil ja 19. sajandi algul. 1. köide. Tallinn, 2003

Hullud, professorid ja müüdud anne / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

2003-01-01

Kurvits, Lembit. Tõrvalill : [luuletused]. Tallinn : Eesti Raamat, 2003 ; Liiv, Toomas. Luuletused 1968-2002. Tallinn : Tuum, 2003 ; Fante, John. Küsi kaduvalt : [romaan / tõlkinud ja järelsõna: Heiti Kender, värsid tõlkinud Mati Soomre. Tallinn] : Hotger, 2003 ; Vinkel, Aarne. Saaremaalt suurele maale. Tallinn : Eesti Keele Sihtasutus, 2003

Bat flight: aerodynamics, kinematics and flight morphology.

Science.gov (United States)

Hedenström, Anders; Johansson, L Christoffer

2015-03-01

Bats evolved the ability of powered flight more than 50 million years ago. The modern bat is an efficient flyer and recent research on bat flight has revealed many intriguing facts. By using particle image velocimetry to visualize wake vortices, both the magnitude and time-history of aerodynamic forces can be estimated. At most speeds the downstroke generates both lift and thrust, whereas the function of the upstroke changes with forward flight speed. At hovering and slow speed bats use a leading edge vortex to enhance the lift beyond that allowed by steady aerodynamics and an inverted wing during the upstroke to further aid weight support. The bat wing and its skeleton exhibit many features and control mechanisms that are presumed to improve flight performance. Whereas bats appear aerodynamically less efficient than birds when it comes to cruising flight, they have the edge over birds when it comes to manoeuvring. There is a direct relationship between kinematics and the aerodynamic performance, but there is still a lack of knowledge about how (and if) the bat controls the movements and shape (planform and camber) of the wing. Considering the relatively few bat species whose aerodynamic tracks have been characterized, there is scope for new discoveries and a need to study species representing more extreme positions in the bat morphospace. © 2015. Published by The Company of Biologists Ltd.

Adjustment of muscle function to flight in bats; Komori no kinkino no hiko eno tekio

Energy Technology Data Exchange (ETDEWEB)

Yamashita, M. [Institute of the Space and Astronautical Science,Tokyo (Japan); Choi, I.H.

1999-12-05

This paper outlines the muscle of bats that generates a motive force for flight. The weight of the muscle is less compared with that of birds. The energy required for flight is twice as much as that for running. Conversely, in view of metabolic cost (transporting cost) for moving a unit mass for a unit distance, the transporting cost of bats for flying is one fifth. The acquisition of this flight ability through evolution can be inferred from the fossils of reptiles. Bats, having a stream-lined body shape and a small body mass, are capable of efficient flight. A fast durable flight is possible by having the pectoral muscle constituted of speed muscles of oxidation/glycolysis muscle fiber, a well-developed oxygen transporting system, the arrangement around the capillary of mitochondria and fat grains that are cell organs for producing energy, and a high-density contact between the capillary and the muscle fiber. The muscle functions at low body temperature and imparts adaptability to hibernation with the body temperature lowered. The flight is controlled by the cycle and synchronized with this biological clock, optical cycle and change in temperature. (NEDO)

Selected Flight Test Results for Online Learning Neural Network-Based Flight Control System

Science.gov (United States)

Williams-Hayes, Peggy S.

2004-01-01

The NASA F-15 Intelligent Flight Control System project team developed a series of flight control concepts designed to demonstrate neural network-based adaptive controller benefits, with the objective to develop and flight-test control systems using neural network technology to optimize aircraft performance under nominal conditions and stabilize the aircraft under failure conditions. This report presents flight-test results for an adaptive controller using stability and control derivative values from an online learning neural network. A dynamic cell structure neural network is used in conjunction with a real-time parameter identification algorithm to estimate aerodynamic stability and control derivative increments to baseline aerodynamic derivatives in flight. This open-loop flight test set was performed in preparation for a future phase in which the learning neural network and parameter identification algorithm output would provide the flight controller with aerodynamic stability and control derivative updates in near real time. Two flight maneuvers are analyzed - pitch frequency sweep and automated flight-test maneuver designed to optimally excite the parameter identification algorithm in all axes. Frequency responses generated from flight data are compared to those obtained from nonlinear simulation runs. Flight data examination shows that addition of flight-identified aerodynamic derivative increments into the simulation improved aircraft pitch handling qualities.

14 CFR 121.412 - Qualifications: Flight instructors (airplane) and flight instructors (simulator).

Science.gov (United States)

2010-01-01

... (airplane) and flight instructors (simulator). 121.412 Section 121.412 Aeronautics and Space FEDERAL... OPERATIONS Training Program § 121.412 Qualifications: Flight instructors (airplane) and flight instructors (simulator). (a) For the purposes of this section and § 121.414: (1) A flight instructor (airplane) is a...

X-36 in Flight over Mojave Desert

Science.gov (United States)

1997-01-01

The unusual lines of the X-36 technology demonstrator contrast sharply with the desert floor as the remotely piloted aircraft scoots across the California desert at low altitude during a research flight on October 30, 1997. The NASA/Boeing X-36 Tailless Fighter Agility Research Aircraft program successfully demonstrated the tailless fighter design using advanced technologies to improve the maneuverability and survivability of possible future fighter aircraft. The program met or exceeded all project goals. For 31 flights during 1997 at the Dryden Flight Research Center, Edwards, California, the project team examined the aircraft's agility at low speed / high angles of attack and at high speed / low angles of attack. The aircraft's speed envelope reached up to 206 knots (234 mph). This aircraft was very stable and maneuverable. It handled very well. The X-36 vehicle was designed to fly without the traditional tail surfaces common on most aircraft. Instead, a canard forward of the wing was used as well as split ailerons and an advanced thrust-vectoring nozzle for directional control. The X-36 was unstable in both pitch and yaw axes, so an advanced, single-channel digital fly-by-wire control system (developed with some commercially available components) was put in place to stabilize the aircraft. Using a video camera mounted in the nose of the aircraft and an onboard microphone, the X-36 was remotely controlled by a pilot in a ground station virtual cockpit. A standard fighter-type head-up display (HUD) and a moving-map representation of the vehicle's position within the range in which it flew provided excellent situational awareness for the pilot. This pilot-in-the-loop approach eliminated the need for expensive and complex autonomous flight control systems and the risks associated with their inability to deal with unknown or unforeseen phenomena in flight. Fully fueled the X-36 prototype weighed approximately 1,250 pounds. It was 19 feet long and three feet high with

Kus me kange bestseller? / Peeter Künstler

Index Scriptorium Estoniae

Künstler, Peeter, 1958-2009

2000-01-01

Arvustus: Uustulnd, Lembit. Kiikhobune Antverpenist. Tallinn : Varrak, 1999 ; Tiidenberg, Ants. Vietnam-transiit Tallinn : SE & JS, 1999 ; Tamman, Tiina. Tihe udu Tallinnas. Tallinn : Perioodika, 2000

Cornerstones at the onset of scientific approach in sports training and physical education in Estonia / Atko Viru

Index Scriptorium Estoniae

Viru, Atko-Meeme, 1932-2007

2003-01-01

Kolmest spordiraamatust: Pihkala, Lauri. Poiste spordi õpetus. Tallinn, 1918 ; Kalamees, Aleksander. Algkooli kehakasvatuse käsiraamat. Tallinn, 1936 ; Kask, Mihkel. Sporditervishoid. Tartu ; Tallinn, 1939

Overview of Pre-Flight Physical Training, In-Flight Exercise Countermeasures and the Post-Flight Reconditioning Program for International Space Station Astronauts

Science.gov (United States)

Kerstman, Eric

2011-01-01

International Space Station (ISS) astronauts receive supervised physical training pre-flight, utilize exercise countermeasures in-flight, and participate in a structured reconditioning program post-flight. Despite recent advances in exercise hardware and prescribed exercise countermeasures, ISS crewmembers are still found to have variable levels of deconditioning post-flight. This presentation provides an overview of the astronaut medical certification requirements, pre-flight physical training, in-flight exercise countermeasures, and the post-flight reconditioning program. Astronauts must meet medical certification requirements on selection, annually, and prior to ISS missions. In addition, extensive physical fitness testing and standardized medical assessments are performed on long duration crewmembers pre-flight. Limited physical fitness assessments and medical examinations are performed in-flight to develop exercise countermeasure prescriptions, ensure that the crewmembers are physically capable of performing mission tasks, and monitor astronaut health. Upon mission completion, long duration astronauts must re-adapt to the 1 G environment, and be certified as fit to return to space flight training and active duty. A structured, supervised postflight reconditioning program has been developed to prevent injuries, facilitate re-adaptation to the 1 G environment, and subsequently return astronauts to training and space flight. The NASA reconditioning program is implemented by the Astronaut Strength, Conditioning, and Rehabilitation (ASCR) team and supervised by NASA flight surgeons. This program has evolved over the past 10 years of the International Space Station (ISS) program and has been successful in ensuring that long duration astronauts safely re-adapt to the 1 g environment and return to active duty. Lessons learned from this approach to managing deconditioning can be applied to terrestrial medicine and future exploration space flight missions.

Mõned mõtted "suvelugemisest" ja suvelugemisest / Peeter Helme

Index Scriptorium Estoniae

Helme, Peeter, 1978-

2009-01-01

Tutvustatakse ja soovitatakse raamatuid: Aleksejev, Tiit. Palveränd : lugu Esimesest ristisõjast. Tallinn : Varrak, 2008 ; Rebane, Kristi. Minu oma. Tallinn : Tänapäev, 2009 ; Kaints, Holger. Lennukivaatleja. Tallinn : Kultuurileht, 2009 ; Kehlmann, Daniel. Maailma mõõtmine. Tartu : Atlex, c2008 ; Zafón, Carlos Ruiz. Tuule vari. Tallinn : Varrak, 2008

Short outlines of books by Estonian authors / Janika Kronberg and Rutt Hinrikus

Index Scriptorium Estoniae

Kronberg, Janika, 1963-

2010-01-01

Arvustus: Kiin, Sirje. Marie Under : elu, luuletaja identiteet ja teoste vastuvõtt. Tallinn : Tänapäev, 2009 ; Laanes, Eneken. Lepitamatud dialoogid : subjekt ja mälu nõukogudejärgses eesti romaanis. Tartu : Tartu Ülikooli Kirjastus, 2009 ; Ehin, Kristiina. Emapuhkus. Tallinn : Pandekt, 2009 ; Tungal, Leelo. Seltsimees laps ja suured inimesed. Tallinn : Tänapäev, 2008 ; Tungal, Leelo. Samet ja saepuru, ehk, Seltsimees laps ja kirjatähed. Tallinn : Tänapäev, 2009 ; Õnnepalu, Tõnu. Paradiis. Tallinn : Varrak, 2009

Role of environment in strengthening competitiveness of cities by example of European Green Capitals and Tallinn

Directory of Open Access Journals (Sweden)

Jüri Ratas

2014-01-01

Full Text Available Guaranteeing a high-level living environment is one of the most important preconditions to the balanced and sustainable economic and social development of the European Union. Serious environmental problems can be seen in European cities, which are the places where most of the population live and which create the highest number of jobs, economic growth and added value. The level of urbanisation in Europe was 72.7% in 2010 and the UN forecast that it will increase to 82.2% by 2050. The European Green Capital Award was created in 2006 in order to recognise cities that have contributed to the improvement of their quality of life. The cities that have won the award have started using the most innovative and efficient measures for increasing the city’s competitiveness, and are an example of how to achieve sustainable development for all cities, not just capitals. The environmental indicators of cities that have won the European Green Capital Award are high. In this article the problem is analysed using the example of Tallinn, the capital of Estonia, which strives for a place among cities with the highest quality of life in Europe. The objective of this article is to analyse the areas of the city’s environmental activities and environmental organisation in the context of increasing competitiveness. The original database used by the author in this article consists of the responses given by the governments of the cities who have already been awarded the title of European Green Capital when asked to describe the impact that applying for and achieving the title had on their cities

Advanced aircraft service life monitoring method via flight-by-flight load spectra

Science.gov (United States)

Lee, Hongchul

This research is an effort to understand current method and to propose an advanced method for Damage Tolerance Analysis (DTA) for the purpose of monitoring the aircraft service life. As one of tasks in the DTA, the current indirect Individual Aircraft Tracking (IAT) method for the F-16C/D Block 32 does not properly represent changes in flight usage severity affecting structural fatigue life. Therefore, an advanced aircraft service life monitoring method based on flight-by-flight load spectra is proposed and recommended for IAT program to track consumed fatigue life as an alternative to the current method which is based on the crack severity index (CSI) value. Damage Tolerance is one of aircraft design philosophies to ensure that aging aircrafts satisfy structural reliability in terms of fatigue failures throughout their service periods. IAT program, one of the most important tasks of DTA, is able to track potential structural crack growth at critical areas in the major airframe structural components of individual aircraft. The F-16C/D aircraft is equipped with a flight data recorder to monitor flight usage and provide the data to support structural load analysis. However, limited memory of flight data recorder allows user to monitor individual aircraft fatigue usage in terms of only the vertical inertia (NzW) data for calculating Crack Severity Index (CSI) value which defines the relative maneuver severity. Current IAT method for the F-16C/D Block 32 based on CSI value calculated from NzW is shown to be not accurate enough to monitor individual aircraft fatigue usage due to several problems. The proposed advanced aircraft service life monitoring method based on flight-by-flight load spectra is recommended as an improved method for the F-16C/D Block 32 aircraft. Flight-by-flight load spectra was generated from downloaded Crash Survival Flight Data Recorder (CSFDR) data by calculating loads for each time hack in selected flight data utilizing loads equations. From

Raamatuid / Juhan Habicht

Index Scriptorium Estoniae

Habicht, Juhan, 1954-

1991-01-01

Tutvustused: Kivisildnik, Sven. Dawa vita. Tallinn : Eesti Raamat, [1991]. Uustulnd, Albert. Acheroni kaldal. Tallinn : Eesti Raamat, 1991. Kivikas, Albert. Nimed marmortahvlil. Tallinn : Eesti Raamat, 1991

Short outlines of books by Estonian authors / Brita Melts and Rutt Hinrikus

Index Scriptorium Estoniae

Melts, Brita

2011-01-01

Arvustus: Vadi, Urmas. Kirjad tädi Annele. Pärnu : Jumalikud Ilmutused, 2010 ; Sommer, Lauri. Kolm yksiklast. Tallinn : Menu Kirjastus, 2010 ; Hargla, Indrek. Apteeker Melchior ja Oleviste mõistatus. Tallinn : Varrak, 2010 ; Hargla, Indrek. Apteeker Melchior ja Rataskaevu viirastus. Tallinn : Varrak, 2010 ; Pihelgas, Carolina. Metsas algavad hääled. Tallinn : Eesti Keele Sihtasutus, 2010

Advanced Transport Operating System (ATOPS) Flight Management/Flight Controls (FM/FC) software description

Science.gov (United States)

Wolverton, David A.; Dickson, Richard W.; Clinedinst, Winston C.; Slominski, Christopher J.

1993-01-01

The flight software developed for the Flight Management/Flight Controls (FM/FC) MicroVAX computer used on the Transport Systems Research Vehicle for Advanced Transport Operating Systems (ATOPS) research is described. The FM/FC software computes navigation position estimates, guidance commands, and those commands issued to the control surfaces to direct the aircraft in flight. Various modes of flight are provided for, ranging from computer assisted manual modes to fully automatic modes including automatic landing. A high-level system overview as well as a description of each software module comprising the system is provided. Digital systems diagrams are included for each major flight control component and selected flight management functions.

Kas keegi vajab neid raamatuid? / Jaanika Palm

Index Scriptorium Estoniae

Palm, Jaanika, 1973-

2001-01-01

Rets. rmt. : Müürsepp, Mare. Kolm põrsakest. Punamütsike : muinasjutu-kirjavihik 5-aastastele lastele. 1 vihik / jutustanud, luuletanud ja ülesanded välja mõelnud Mare Müürsepp. Tallinn : Ilo, 2000. Sari "Muinasjutt õpetab" : Hans ja Grete / [idee: Nicole Lenaerts-Viroux. Tallinn] : Egmont Estonia, 2001; Hunt ja seitse kitsetalle / [idee: Nicole Lenaerts-Viroux. Tallinn] : Egmont Estonia, 2000; Lumivalgeke ja seitse pöialpoissi / [idee: Nicole Lenaerts-Viroux. Tallinn] : Egmont Estonia, 2001; Pöial-Liisi / [idee: Nicole Lenaerts-Viroux. Tallinn] : Egmont Estonia, 2000

Maailmalapsed / Janika Kronberg

Index Scriptorium Estoniae

Kronberg, Janika, 1963-

1997-01-01

Sisu: Kareva, Doris. Hingring. Tallinn : Huma, 1997; Kareva, Doris; Tervonen, Marina. Kammertoon. [Tallinn] : D. Kareva ; M. Tervonen, 1997; Gibran, Kahlil. Prohvet / tlk. Doris Kareva. Tallinn : Huma, 1997

Time-of-flight spectrometer for the measurement of gamma correlated neutron spectra

International Nuclear Information System (INIS)

Andriashin, A.V.; Devkin, B.V.; Lychagin, A.A.; Minko, J.V.; Mironov, A.N.; Nesterenko, V.S.; Sztaricskai, T.; Petoe, G.; Vasvary, L.

1986-01-01

A time-of-flight spectrometer for the measurement of gamma correlated neutron spectra from (n,xnγ) reactions is described. The operation and the main parameters are discussed. The resolution in the neutron channel is 2.2 ns/m at the 150 keV neutron energy threshold. A simultaneous measurement of the time-of-flight and amplitude distributions makes it possible to study gamma correlated neutron spectra as well as the prompt gamma spectra in coincidence with selected energy neutrons. In order to test the spectrometer, measurements of the neutron spectrum in coincidence with the 846 keV gamma line of 56 Fe were carried out at an incident neutron energy of 14.1 MeV. (Auth.)

On teil mõnda seksiga raamatut kah? / Tauno Vahter

Index Scriptorium Estoniae

Vahter, Tauno

2001-01-01

Arvustus: Bukowski, Charles. Naised / inglise k. tlk. Peeter Sauter. Tallinn : Hotger, 2001 ; Bukowski, Charles. Postkontor / inglise k. tlk. Kaur Kender. Tallinn : Hotger, 2001 ; Jerofejev, Venedikt. Moskva-Petushki / vene k. tlk. Ott Arder. 2. tr. Tallinn Tänapäev, 2001 ; Jerofejev, Venedikt. Psühhopaadi märkmed / vene k. tlk. Igor Kurve. Tallinn : Tänapäev, 2001

[Jacqueline Wilson. Tracy Beakeri sari] / Krista Kivisalu

Index Scriptorium Estoniae

Kivisalu, Krista, 1968-

2016-01-01

Tutvustus: Wilson, Jacqueline. Tracy Beakeri lugu. [Tallinn] : Pegasus, 2015 ; Wilson, Jacqueline. Pühadeüllatus. [Tallinn] : Pegasus, c2015 ; Wilson, Jacqueline. Julgusmäng. [Tallinn] : Pegasus, c2015

Raamatud / Juhan Habicht

Index Scriptorium Estoniae

Habicht, Juhan, 1954-

1991-01-01

Raamatutvustused: Beier, Priidu. Mustil päevil. Tallinn : Eesti Raamat, [1991]. Ristikivi, Karl. Inimese teekond : luuletusi. Tallinn : Eesti Raamat, 1991. Erich, Artur. Äike. Tallinn : Eesti Raamat, [1991

Ladina keele õpikud ja sententsikogumikud / Ivo Volt

Index Scriptorium Estoniae

Volt, Ivo, 1975-

2000-01-01

Ka sententsikogumikest: V. Hromov. Dicta et proverbia Latina. Tallinn : Perioodika, 1997 ; 1001 ladina sententsi eesti vastetega. Tallinn : Valgus, 1997 ; K. Türk. Lendsõnade leksikon. Tallinn : Avita, 1998

Computational imaging with multi-camera time-of-flight systems

KAUST Repository

Shrestha, Shikhar

2016-07-11

Depth cameras are a ubiquitous technology used in a wide range of applications, including robotic and machine vision, human computer interaction, autonomous vehicles as well as augmented and virtual reality. In this paper, we explore the design and applications of phased multi-camera time-of-flight (ToF) systems. We develop a reproducible hardware system that allows for the exposure times and waveforms of up to three cameras to be synchronized. Using this system, we analyze waveform interference between multiple light sources in ToF applications and propose simple solutions to this problem. Building on the concept of orthogonal frequency design, we demonstrate state-of-the-art results for instantaneous radial velocity capture via Doppler time-of-flight imaging and we explore new directions for optically probing global illumination, for example by de-scattering dynamic scenes and by non-line-of-sight motion detection via frequency gating. © 2016 ACM.

In-flight spectral performance monitoring of the Airborne Prism Experiment.

Science.gov (United States)

D'Odorico, Petra; Alberti, Edoardo; Schaepman, Michael E

2010-06-01

Spectral performance of an airborne dispersive pushbroom imaging spectrometer cannot be assumed to be stable over a whole flight season given the environmental stresses present during flight. Spectral performance monitoring during flight is commonly accomplished by looking at selected absorption features present in the Sun, atmosphere, or ground, and their stability. The assessment of instrument performance in two different environments, e.g., laboratory and airborne, using precisely the same calibration reference, has not been possible so far. The Airborne Prism Experiment (APEX), an airborne dispersive pushbroom imaging spectrometer, uses an onboard in-flight characterization (IFC) facility, which makes it possible to monitor the sensor's performance in terms of spectral, radiometric, and geometric stability in flight and in the laboratory. We discuss in detail a new method for the monitoring of spectral instrument performance. The method relies on the monitoring of spectral shifts by comparing instrument-induced movements of absorption features on ground and in flight. Absorption lines originate from spectral filters, which intercept the full field of view (FOV) illuminated using an internal light source. A feature-fitting algorithm is used for the shift estimation based on Pearson's correlation coefficient. Environmental parameter monitoring, coregistered on board with the image and calibration data, revealed that differential pressure and temperature in the baffle compartment are the main driving parameters explaining the trend in spectral performance deviations in the time and the space (across-track) domains, respectively. The results presented in this paper show that the system in its current setup needs further improvements to reach a stable performance. Findings provided useful guidelines for the instrument revision currently under way. The main aim of the revision is the stabilization of the instrument for a range of temperature and pressure conditions

Gollandskaja KLM natshinajet poljotõ v Amsterdam / Diana King

Index Scriptorium Estoniae

King, Diana

2005-01-01

Tallinnast alustasid liinilende esmakordselt Eesti turule saabunud lennufirmad: Hollandi KML alustas regulaarlende Tallinn-Amsterdami liinil ning Rootsi tütarfirma Finnair-flyNordic Tallinn-Stockholmi ja Tallinn-Kopenhaageni liinil

Ulmekaravan liigub / Veiko Belials

Index Scriptorium Estoniae

Belials, Veiko, 1966-

2001-01-01

Arvustus: Hargla, Indrek. Pan Grpowski üheksa juhtumit. Tallinn : Kuldsulg, 2001 ; Berg, Lew R. Tempel selvas. Tallinn : Salasõna, 2001 ; Veskimees, Siim. Operatsioon "Ogaline Päike. Tallinn : Fantaasia, 2001

Silmakirjalik aastasada / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

2006-01-01

Tutvustus: Hyvärinen, Pekka. Soome mees : Urho Kekkose elu / tlk. Tauno Vahter. Tallinn : Tänapäev, 2006 ; Tuchman, Barbara W. Augustikahurid / tlk. Armand Tungal ja Tõnis Värnik. Tallinn : Varrak, 2006 ; Ernesaks, Viive. Viiv. Tallinn : Varrak, 2006 ; Kiik, Heino. Leida ennast : 1954-1963. Viies raamat. Tartu : Ilmamaa, 2006 ; Lotman, Juri. Vestlusi vene kultuurist : Vene aadli argielu ja traditsioonid 18. sajandil ja 19. sajandi algul. 2 / [tõlkinud Kajar Pruul]. Tallinn : Tänapäev, 2006 ; Lotman, Mihhail. Pistriku talvekarje : esseid Joseph Brodsky poeetikast ja surmast. Tallinn : Varrak, 2005

COINTOF mass spectrometry: design of a time-of-flight analyzer and development of the analysis method

International Nuclear Information System (INIS)

Teyssier, C.

2012-01-01

DIAM (Device for the irradiation of molecular clusters) is a newly designed experimental setup to investigate processes resulting from the irradiation of molecular nano-systems by 20-150 keV protons. One of its specificities relies on the original technique of mass spectrometry named COINTOF (Correlated Ion and Neutral Time Of Flight) consisting in correlated measurements of the time of flight of charged and neutral fragments produced by the dissociation of a single molecular ion parent. A strategy of treatment and analysis of the detection signals was developed to distinguish two fragments close in time ( 3 O + and two water molecules. The distribution of the time of flight difference between the two neutral fragments is measured providing an estimate of the kinetic energy release of a few eV. In parallel, a second time-of-flight mass spectrometer was designed. It associates a linear time-of-flight and an orthogonal time-of-flight and integrates position detectors (delay line anode). Simulations demonstrate the potentials of the new analyzer. Finally, research works were led at the laboratory R.-J. A. Levesque (Universite de Montreal) on the imaging capabilities of the multi-pixel detectors of the MPX-ATLAS collaboration. (author)

Apteeginaps ajaloomälu turgutuseks / Aet Varik

Index Scriptorium Estoniae

Varik, Aet

2011-01-01

Arvustus: Hargla, Indrek. Apteeker Melchior ja Oleviste mõistatus. Tallinn : Varrak, 2010 ; Apteeker Melchior ja Rataskaevu viirastus. Tallinn : Varrak, 2010 ; Apteeker Melchior ja timuka tütar. Tallinn : Varrak, 2011

Kuula ka neid / Joosep Sang

Index Scriptorium Estoniae

Sang, Joosep

2009-01-01

Tutvustused : XXI Sajandi Orkester. Üheksa. Tallinn : XXISO, 2008. Illustraator. Minu keha. Tallinn : MTÜ ILL Produktsioon, 2008. Pastoraal. Helirännak põldudel ja heinamaadel. Tallinn : Eestimaa Looduse fond, 2008

Flight Planning

Science.gov (United States)

1991-01-01

Seagull Technology, Inc., Sunnyvale, CA, produced a computer program under a Langley Research Center Small Business Innovation Research (SBIR) grant called STAFPLAN (Seagull Technology Advanced Flight Plan) that plans optimal trajectory routes for small to medium sized airlines to minimize direct operating costs while complying with various airline operating constraints. STAFPLAN incorporates four input databases, weather, route data, aircraft performance, and flight-specific information (times, payload, crew, fuel cost) to provide the correct amount of fuel optimal cruise altitude, climb and descent points, optimal cruise speed, and flight path.

Lugemisnoppeid: antropoloogia / Marek Tamm

Index Scriptorium Estoniae

Tamm, Marek, 1973-

2012-01-01

Tutvustus: Jürgenson, Aivar. Ladina rahva seas : Argentina ja sealsed eestlased. Tallinn, 2011 ; Annist, Aet. Otsides kogukonda sotsialismijärgses keskuskülas : arenguantropoloogiline uurimus. Tallinn : Tallinna Ülikooli Kirjastus, 2011. (Acta Universitatis Tallinnensis. Socialia) ; Hiiemäe, Reet. Kaitsemaagia eesti rahvausundis. Tallinn, 2012 ; Augé, Marc. Kohad ja mittekohad : sissejuhatus ülimodernsuse antropoloogiasse. Tallinn : Tallinna Ülikooli Kirjastus, 2012. (Bibliotheca controversiarum)

An adaptive dual-optimal path-planning technique for unmanned air vehicles with application to solar-regenerative high altitude long endurance flight

Science.gov (United States)

Whitfield, Clifford A.

2009-12-01

A multi-objective technique for Unmanned Air Vehicle (UAV) path and trajectory autonomy generation, through task allocation and sensor fusion has been developed. The Dual-Optimal Path-Planning (D-O.P-P.) Technique generates on-line adaptive flight paths for UAVs based on available flight windows and environmental influenced objectives. The environmental influenced optimal condition, known as the driver' determines the condition, within a downstream virtual window of possible vehicle destinations and orientation built from the UAV kinematics. The intermittent results are pursued by a dynamic optimization technique to determine the flight path. This sequential optimization technique is a multi-objective optimization procedure consisting of two goals, without requiring additional information to combine the conflicting objectives into a single-objective. An example case-study and additional applications are developed and the results are discussed; including the application to the field of Solar Regenerative (SR) High Altitude Long Endurance (HALE) UAV flight. Harnessing solar energy has recently been adapted for use on high altitude UAV platforms. An aircraft that uses solar panels and powered by the sun during the day and through the night by SR systems, in principle could sustain flight for weeks or months. The requirements and limitations of solar powered flight were determined. The SR-HALE UAV platform geometry and flight characteristics were selected from an existing aircraft that has demonstrated the capability for sustained flight through flight tests. The goals were to maintain continual Situational Awareness (SA) over a case-study selected Area of Interest (AOI) and existing UAV power and surveillance systems. This was done for still wind and constant wind conditions at altitude along with variations in latitude. The characteristics of solar flux and the dependence on the surface location and orientation were established along with fixed flight maneuvers for

Three Women in Quest of Narrative / Tiina Kirss

Index Scriptorium Estoniae

Kirss, Tiina, 1957-

2008-01-01

Epp Annuse romaanist "Sina, Matilda" (Tallinn : Tuum, 2007), Kärt Hellermaa novellikogust "Ma armastasin David Copperfieldi" (Tallinn : Tuum, 2007) ja Kristiina Ehini lühiproosakogust "Pillipuhujanaine ja pommipanijanaine" (Tallinn : Huma, 2006)

Jaan Ellen talletab rahva valu / Contra

Index Scriptorium Estoniae

Contra, pseud., 1974-

2005-01-01

Raamatud : Ellen, Jaan. Hällimaa. Tallinn, 2004 ; Varjatud valu : mälestusi Teisest maailmasõjast / koostaja Jaan Ellen. Tallinn, 2005 ; Palutedre, Arnold-Johannes. Viis tuhat päeva : [memuaarid]. Tallinn, 2005

Jaan Ellen loob ehedaid elupilte eesti rahva saatusest / Liina Valper

Index Scriptorium Estoniae

Valper, Liina, 1941-

2005-01-01

Raamatud : Ellen, Jaan. Hällimaa. Tallinn, 2004 ; Varjatud valu : mälestusi Teisest maailmasõjast / koostaja Jaan Ellen. Tallinn, 2005 ; Palutedre, Arnold-Johannes. Viis tuhat päeva : [memuaarid]. Tallinn, 2005

Maffia, hullus ja Sannikovi maa / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

2011-01-01

Arvustus: Roberts, Gregory David. Shantaram. 1.-2. raamat / tõlkinud Riina Jesmin. Tallinn : Varrak, 2011 ; Akutagawa, Ryūnosuke. Mandariinid tihnikus. Tallinn : Varrak, 2011 ; Põder, Rein. Kauge. Tallinn : Eesti Raamat, 2011

Oliivipuude triloogia - mõnus suvine võrkkiige-lugemine / Mari Klein

Index Scriptorium Estoniae

Klein, Mari

2007-01-01

Tutvustus: Drinkwater, Carol. Oliiviistandus / tlk. Laine Hone. Tallinn : Varrak, 2004 ; Drinkwater, Carol. Oliivisaak / tlk. Eve-Reet Tammet. Tallinn : Varrak, 2997 ; Drinkwater, Carol. Oliivihooaeg / tlk. Lane Hone ja Karin Rita. Tallinn : Varrak, 2006

Kliiniline kapitalism ja naise neim / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

2011-01-01

Tutvustus: Kõiv, Salme. Reet Tammiku. Tallinn : Eesti Raamat, 2011 ; Kalda, Katrin. Eesti romaan / tõlkinud Anti Saar. Tallinn : Varrak, 2011 ; Zola, Émile. Saak / tõlkinud Kaja Riesen. Tallinn : Eesti Raamat, 2011

Põnevikud kõige väiksematele / Krista Kumberg

Index Scriptorium Estoniae

Kumberg, Krista, 1959-

2006-01-01

Arvustus: Tungal, Leelo. Siil Felix ja kriminaalne loomaaed. Tallinn : Varrak, 2005 ; Tungal, Leelo. Siil Felix ja sekelduste sügis. Tallinn : Varrak, 2005 ; Tungal, Leelo. Hernetont Ernestiine. Tallinn : Eesti Entsüklopeediakirjastus, 2005.

Advanced transport operating system software upgrade: Flight management/flight controls software description

Science.gov (United States)

Clinedinst, Winston C.; Debure, Kelly R.; Dickson, Richard W.; Heaphy, William J.; Parks, Mark A.; Slominski, Christopher J.; Wolverton, David A.

1988-01-01

The Flight Management/Flight Controls (FM/FC) software for the Norden 2 (PDP-11/70M) computer installed on the NASA 737 aircraft is described. The software computes the navigation position estimates, guidance commands, those commands to be issued to the control surfaces to direct the aircraft in flight based on the modes selected on the Advanced Guidance Control System (AGSC) mode panel, and the flight path selected via the Navigation Control/Display Unit (NCDU).

[Raamatututvustused] / Ervin Õunapuu

Index Scriptorium Estoniae

Õunapuu, Ervin, 1956-

2007-01-01

Tutvustus: Remarque, Erich Maria. Lissaboni öö. Tallinn : Tänapäev, 2006 ; Jõgisalu, Harri, Tihkan, Lembit. Tulihända püüdmas : lugusid vanalt Läänemaalt. Tallinn : Eesti Raamat, 2001 // Kivirähk, Andrus. Mees, kes teadis ussisõnu. Tallinn : Eesti Keele Sihtasutus, 2007 // Raud, Eno. Tallinn : Ilo, 2005 // Tammsaare, A. H. Sic transit... : kas seni teadlikult "unustatud"?. Muraste : Matrix Kirjastus, 2004

Short outlines of books by Estonian authors / Brita Melts, Rutt Hinrikus and Janika Kronberg

Index Scriptorium Estoniae

Melts, Brita

2015-01-01

Arvustus: Afanasjev, Vahur. Tünsamäe tigu. Tartu Tartu NAK, 2015 ; Vadi, Urmas. Kuidas me kõik reas niimoodi läheme. Tallinn : Tuum, 2014 ; Traat, Mats. Kolm Solveigi. Tartu : Ilmamaa, 2015 ; Saat, Mari. Matused ja laulupeod. Tartu : Petrone Print, 2015 ; Kivisilla, Veronika. Cantus firmus. Tallinn : Näo Kirik, 2015 ; Kolk, Jüri. Suur võidujooks. Tallinn : Tuum, 2015 ; Mudlum. Tõsine inimene. Tallinn : ZA/UM, 2014

Free Flight Ground Testing of ADEPT in Advance of the Sounding Rocket One Flight Experiment

Science.gov (United States)

Smith, B. P.; Dutta, S.

2017-01-01

The Adaptable Deployable Entry and Placement Technology (ADEPT) project will be conducting the first flight test of ADEPT, titled Sounding Rocket One (SR-1), in just two months. The need for this flight test stems from the fact that ADEPT's supersonic dynamic stability has not yet been characterized. The SR-1 flight test will provide critical data describing the flight mechanics of ADEPT in ballistic flight. These data will feed decision making on future ADEPT mission designs. This presentation will describe the SR-1 scientific data products, possible flight test outcomes, and the implications of those outcomes on future ADEPT development. In addition, this presentation will describe free-flight ground testing performed in advance of the flight test. A subsonic flight dynamics test conducted at the Vertical Spin Tunnel located at NASA Langley Research Center provided subsonic flight dynamics data at high and low altitudes for multiple center of mass (CoM) locations. A ballistic range test at the Hypervelocity Free Flight Aerodynamics Facility (HFFAF) located at NASA Ames Research Center provided supersonic flight dynamics data at low supersonic Mach numbers. Execution and outcomes of these tests will be discussed. Finally, a hypothesized trajectory estimate for the SR-1 flight will be presented.

Short outlines of books by Estonian authors / Janika Kronberg, Rutt Hinrikus

Index Scriptorium Estoniae

Kronberg, Janika, 1963-

2006-01-01

Arvustus: Runnel, Hando. Sinamu. Tartu : Ilmamaa, 2005 ; Talvet, Jüri. Tõrjumatu äär. Tartu : Ilmamaa, 2005 ; Nõu, Enn. Mõtusekuke viimne kogupauk. Tallinn : Eesti Keele Sihtasutus, 2005 ; Merca. Hele häärber. Tartu : Vilep & Vallik, 2005 ; Õnnepalu, Tõnu. Enne heinaaega ja hiljem : luulet ja luuletõlkeid 1983-2005. Tallinn : Eesti Keele Sihtasutus, 2005 ; Kaplinski, Jaan. Kõik on ime. Tartu : Ilmamaa, 2004 ; Unt, Mati. Vend Antigone, ema Oidipus. Tallinn : Kultuurileht, 2006 ; Laretei, Käbi. Otsekui tõlkes : teema variatsioonidega. Tallinn : Tänapäev, 2005 ; Jõerüüt, Jaak. Sõber : valik novelle 1979-2005. Tallinn : Tuum, 2005

Tumedad ained kirjanduses ja päriselt / Mare Müürsepp

Index Scriptorium Estoniae

Müürsepp, Mare

2007-01-01

Analüüsitud on Philip Pullmani triloogiasse "Tema tumedad ained" kuuluvaid romaane : Pullman, Philip. Kuldne kompass. Tallinn : Tiritamm, 2002; Pullman, Philip. Inglite torn. Tallinn : Tiritamm, 2004; Pullman, Philip. Vaigust kiiker. Tallinn : Tiritamm, 2005

[Eve Hele Sits. Mooni talurahva tähtpäevik ; Mooni metsauudistaja ; Mooni Eestimaa raamat ] / Helja Kirber ; suomennos Katariina Suurpalo

Index Scriptorium Estoniae

Kirber, Helja

2014-01-01

Tutvustus: Sits, Eve Hele. Mooni talurahva tähtpäevik. [Tallinn] : Argo, c2011; Mooni metsauudistaja : tähelepanekuid ja lugusid metsaelust. [Tallinn] : Argo, c2012; Mooni Eestimaa raamat. [Tallinn] : Argo, c2013

Kolm Goncourt'i laureaati korraga / Marek Tamm

Index Scriptorium Estoniae

Tamm, Marek, 1973-

2002-01-01

Arvustus: Tournier, Michel. Haldjakuningas / tlk. Laine Hone. Tallinn : Eesti Raamat, 2002 ; Rouaud, Jean. Auväljad / tlk. Vladimir Indrikson. Tallinn : Atlantis, 2002 ; Roze, Pascale. Hävituslendur Zéro / tlk. Kaja Riesen. Tallinn : Olion, 2002

Eesti vajab oma Richelieu'd / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

2006-01-01

Tutvustus: Faulkner, William. Sartoris / tõlkinud Vilma Jürisalu. Tallinn : Eesti Raamat, 2005 ; Runnel, Hando. Sinamu. Tartu : Ilmamaa, 2005 ; Levi, Anthony. Richelieu. Tallinn : Varrak, 2005 ; Lõvi, Oskar. Kolm naist [1-3]. Tallinn : Varrak, 2005

Flight control actuation system

Science.gov (United States)

Wingett, Paul T. (Inventor); Gaines, Louie T. (Inventor); Evans, Paul S. (Inventor); Kern, James I. (Inventor)

2006-01-01

A flight control actuation system comprises a controller, electromechanical actuator and a pneumatic actuator. During normal operation, only the electromechanical actuator is needed to operate a flight control surface. When the electromechanical actuator load level exceeds 40 amps positive, the controller activates the pneumatic actuator to offset electromechanical actuator loads to assist the manipulation of flight control surfaces. The assistance from the pneumatic load assist actuator enables the use of an electromechanical actuator that is smaller in size and mass, requires less power, needs less cooling processes, achieves high output forces and adapts to electrical current variations. The flight control actuation system is adapted for aircraft, spacecraft, missiles, and other flight vehicles, especially flight vehicles that are large in size and travel at high velocities.

Time-of-flight spectrometer for the measurement of gamma correlated neutron spectra

International Nuclear Information System (INIS)

Andryashin, A.V.; Devlein, B.V.; Lychagin, A.A.; Minko, Y.V.; Mironov, A.N.; Nesterenko, V.S.

1986-01-01

A time-of-flight spectrometer for the measurement of gamma correlated neutron spectra form (n,xnγ) reactions is described. The operation and the main parameters are discussed. The resolution in the neutron channel is 2.2 ns/m at the 150 keV neutron energy threshold. A simultaneous measurement of the time-of-flight and amplitude distributions makes it possible to study gamma correlated neutron spectra as well as the prompt gamma spectra in coincidence with selected energy neutrons. In order to test the spectrometer, measurements of the neutron spectrum in coincidence with the 846 keV gamma line of 56 Fe were carried out at an incident neutron energy of 14.1 MeV. (author). 3 figs., 6 refs

Aurora Flight Sciences' Perseus B Remotely Piloted Aircraft in Flight

Science.gov (United States)

1998-01-01

A long, slender wing and a pusher propeller at the rear characterize the Perseus B remotely piloted research aircraft, seen here during a test flight in June 1998. Perseus B is a remotely piloted aircraft developed as a design-performance testbed under NASA's Environmental Research Aircraft and Sensor Technology (ERAST) project. Perseus is one of several flight vehicles involved in the ERAST project. A piston engine, propeller-powered aircraft, Perseus was designed and built by Aurora Flight Sciences Corporation, Manassas, Virginia. The objectives of Perseus B's ERAST flight tests have been to reach and maintain horizontal flight above altitudes of 60,000 feet and demonstrate the capability to fly missions lasting from 8 to 24 hours, depending on payload and altitude requirements. The Perseus B aircraft established an unofficial altitude record for a single-engine, propeller-driven, remotely piloted aircraft on June 27, 1998. It reached an altitude of 60,280 feet. In 1999, several modifications were made to the Perseus aircraft including engine, avionics, and flight-control-system improvements. These improvements were evaluated in a series of operational readiness and test missions at the Dryden Flight Research Center, Edwards, California. Perseus is a high-wing monoplane with a conventional tail design. Its narrow, straight, high-aspect-ratio wing is mounted atop the fuselage. The aircraft is pusher-designed with the propeller mounted in the rear. This design allows for interchangeable scientific-instrument payloads to be placed in the forward fuselage. The design also allows for unobstructed airflow to the sensors and other devices mounted in the payload compartment. The Perseus B that underwent test and development in 1999 was the third generation of the Perseus design, which began with the Perseus Proof-Of-Concept aircraft. Perseus was initially developed as part of NASA's Small High-Altitude Science Aircraft (SHASA) program, which later evolved into the ERAST

3Corners of the World / Joosep Sang

Index Scriptorium Estoniae

Sang, Joosep

2009-01-01

Arvustused : Robert Jürjendal, Petri Kuljuntausta, David Rothenberg. 3Corners of the World. [Tallinn] : Terra Nova Music, 2008. Nadia ja Fragile. Uhke ali. [Tallinn] : Nadia & Fragile, 2008. UMA. Civitas Soli. [Tallinn] : Elwood, 2008. Uutest heliplaatidest

Kolm, keda miski ei seo / Veiko Märka

Index Scriptorium Estoniae

Märka, Veiko, 1964-

2004-01-01

Arvustus: Jõerüüt, Jaak. Uus raamat : [luuletused]. Tallinn : Tuum, 2004 ; Maiste, Juhan. In Arcadia ego : [luuletused]. Tallinn : J. Maiste, 2004 ; Essa, Maario. Kellegi teise muru : debüütluulekogu. Tallinn : SE & JS, 2004 ;

Ilusast eesti keelest / Ruth Mägi

Index Scriptorium Estoniae

Mägi, Ruth, 1974-

2008-01-01

Kirjastuse TEA sõnaraamatutest: TEA koolisõnastik : eesti keel. Tallinn : TEA Kirjastus, 2008 ; TEA eesti keele rahvasõnaraamat koos õigekirjareeglitega. Tallinn : TEA Kirjastus, 2008 ; TEA rahvasõnaraamat : võõrsõnad. Tallinn : TEA Kirjastus, 2006

Flight Testing an Iced Business Jet for Flight Simulation Model Validation

Science.gov (United States)

Ratvasky, Thomas P.; Barnhart, Billy P.; Lee, Sam; Cooper, Jon

2007-01-01

A flight test of a business jet aircraft with various ice accretions was performed to obtain data to validate flight simulation models developed through wind tunnel tests. Three types of ice accretions were tested: pre-activation roughness, runback shapes that form downstream of the thermal wing ice protection system, and a wing ice protection system failure shape. The high fidelity flight simulation models of this business jet aircraft were validated using a software tool called "Overdrive." Through comparisons of flight-extracted aerodynamic forces and moments to simulation-predicted forces and moments, the simulation models were successfully validated. Only minor adjustments in the simulation database were required to obtain adequate match, signifying the process used to develop the simulation models was successful. The simulation models were implemented in the NASA Ice Contamination Effects Flight Training Device (ICEFTD) to enable company pilots to evaluate flight characteristics of the simulation models. By and large, the pilots confirmed good similarities in the flight characteristics when compared to the real airplane. However, pilots noted pitch up tendencies at stall with the flaps extended that were not representative of the airplane and identified some differences in pilot forces. The elevator hinge moment model and implementation of the control forces on the ICEFTD were identified as a driver in the pitch ups and control force issues, and will be an area for future work.

Flight research and testing

Science.gov (United States)

Putnam, Terrill W.; Ayers, Theodore G.

1989-01-01

Flight research and testing form a critical link in the aeronautic research and development chain. Brilliant concepts, elegant theories, and even sophisticated ground tests of flight vehicles are not sufficient to prove beyond a doubt that an unproven aeronautical concept will actually perform as predicted. Flight research and testing provide the ultimate proof that an idea or concept performs as expected. Ever since the Wright brothers, flight research and testing were the crucible in which aeronautical concepts were advanced and proven to the point that engineers and companies are willing to stake their future to produce and design aircraft. This is still true today, as shown by the development of the experimental X-30 aerospace plane. The Dryden Flight Research Center (Ames-Dryden) continues to be involved in a number of flight research programs that require understanding and characterization of the total airplane in all the aeronautical disciplines, for example the X-29. Other programs such as the F-14 variable-sweep transition flight experiment have focused on a single concept or discipline. Ames-Dryden also continues to conduct flight and ground based experiments to improve and expand the ability to test and evaluate advanced aeronautical concepts. A review of significant aeronautical flight research programs and experiments is presented to illustrate both the progress being made and the challenges to come.

14 CFR 25.865 - Fire protection of flight controls, engine mounts, and other flight structure.

Science.gov (United States)

2010-01-01

... 14 Aeronautics and Space 1 2010-01-01 2010-01-01 false Fire protection of flight controls, engine... Design and Construction Fire Protection § 25.865 Fire protection of flight controls, engine mounts, and other flight structure. Essential flight controls, engine mounts, and other flight structures located in...

Aino Kalda päevikud : Valgus ja varjud ; Valguse ja varju segu ; Hingesillad ; Rikas, kuhjaga täis / Hilve Rebane

Index Scriptorium Estoniae

Rebane, Hilve, 1938-2012

2003-01-01

Arvustus: Kallas, Aino. Pärjapunuja. Päevaraamat aastaist 1897-1900. Tallinn : Eesti Raamat, 1994 ; Kallas, Aino. Jäätunud šampanja. Päevaraamat aastaist 1907-1915. Tallinn : Eesti Raamat, 1994 ; Kallas, Aino. Hingesild. Päevikulehti aastaist 1916-1921. Tallinn : Eesti Raamat, 1993 ; Kallas, Aino. Suurlinnade udus ja säras. Päevaraamat aastaist 1922-1926. Tallinn : Eesti Raamat, 1996 ; Kallas, Aino. Pööripäevad. Päevaraamat aastaist 1927-1931

L(sub 1) Adaptive Flight Control System: Flight Evaluation and Technology Transition

Science.gov (United States)

Xargay, Enric; Hovakimyan, Naira; Dobrokhodov, Vladimir; Kaminer, Isaac; Gregory, Irene M.; Cao, Chengyu

2010-01-01

Certification of adaptive control technologies for both manned and unmanned aircraft represent a major challenge for current Verification and Validation techniques. A (missing) key step towards flight certification of adaptive flight control systems is the definition and development of analysis tools and methods to support Verification and Validation for nonlinear systems, similar to the procedures currently used for linear systems. In this paper, we describe and demonstrate the advantages of L(sub l) adaptive control architectures for closing some of the gaps in certification of adaptive flight control systems, which may facilitate the transition of adaptive control into military and commercial aerospace applications. As illustrative examples, we present the results of a piloted simulation evaluation on the NASA AirSTAR flight test vehicle, and results of an extensive flight test program conducted by the Naval Postgraduate School to demonstrate the advantages of L(sub l) adaptive control as a verifiable robust adaptive flight control system.

Time- and energy resolved photoemission electron microscopy-imaging of photoelectron time-of-flight analysis by means of pulsed excitations

International Nuclear Information System (INIS)

Oelsner, Andreas; Rohmer, Martin; Schneider, Christian; Bayer, Daniela; Schoenhense, Gerd; Aeschlimann, Martin

2010-01-01

The present work enlightens the developments in time- and energy resolved photoemission electron microscopy over the past few years. We describe basic principles of the technique and demonstrate different applications. An energy- and time-filtering photoemission electron microscopy (PEEM) for real-time spectroscopic imaging can be realized either by a retarding field or hemispherical energy analyzer or by using time-of-flight optics with a delay line detector. The latter method has the advantage of no data loss at all as all randomly incoming particles are measured not only by position but also by time. This is of particular interest for pump-probe experiments in the femtosecond and attosecond time scale where space charge processes drastically limit the maximum number of photoemitted electrons per laser pulse. This work focuses particularly on time-of-flight analysis using a novel delay line detector. Time and energy resolved PEEM instruments with delay line detectors enable 4D imaging (x, y, Δt, E Kin ) on a true counting basis. This allows a broad range of applications from real-time observation of dynamic phenomena at surfaces to fs time-of-flight spectro-microscopy and even aberration correction. By now, these time-of-flight analysis instruments achieve intrinsic time resolutions of 108 ps absolute and 13.5 ps relative. Very high permanent measurement speeds of more than 4 million events per second in random detection regimes have been realized using a standard USB2.0 interface. By means of this performance, the time-resolved PEEM technique enables to display evolutions of spatially resolved (<25 nm) and temporal sliced images life on any modern computer. The method allows dynamics investigations of variable electrical, magnetic, and optical near fields at surfaces and great prospects in dynamical adaptive photoelectron optics. For dynamical processes in the ps time scale such as magnetic domain wall movements, the time resolution of the delay line detectors

Insect Flight: From Newton's Law to Neurons

Science.gov (United States)

Wang, Z. Jane

2016-03-01

Why do animals move the way they do? Bacteria, insects, birds, and fish share with us the necessity to move so as to live. Although each organism follows its own evolutionary course, it also obeys a set of common laws. At the very least, the movement of animals, like that of planets, is governed by Newton's law: All things fall. On Earth, most things fall in air or water, and their motions are thus subject to the laws of hydrodynamics. Through trial and error, animals have found ways to interact with fluid so they can float, drift, swim, sail, glide, soar, and fly. This elementary struggle to escape the fate of falling shapes the development of motors, sensors, and mind. Perhaps we can deduce parts of their neural computations by understanding what animals must do so as not to fall. Here I discuss recent developments along this line of inquiry in the case of insect flight. Asking how often a fly must sense its orientation in order to balance in air has shed new light on the role of motor neurons and steering muscles responsible for flight stability.

[Raamat] / Elina Kalm

Index Scriptorium Estoniae

Kalm, Elina

2007-01-01

Tutvustus: Stroud, Jonathan. Samarkandi amulett / tlk. Bibi Raid. Tallinn : Pegasus, 2005 ; Stroud, Jonathan. Golemi silm / tlk. Bibi Raid. Tallinn : Pegasus, 2007 ; Stroud, Jonathan. Ptolemaiose värav / tlk. Bibi Raid. Tallinn : Pegasus, 2007. (Bartimaeuse triloogia ; 1-3)

Coiled transmission line pulse generators

Science.gov (United States)

McDonald, Kenneth Fox

2010-11-09

Methods and apparatus are provided for fabricating and constructing solid dielectric "Coiled Transmission Line" pulse generators in radial or axial coiled geometries. The pour and cure fabrication process enables a wide variety of geometries and form factors. The volume between the conductors is filled with liquid blends of monomers, polymers, oligomers, and/or cross-linkers and dielectric powders; and then cured to form high field strength and high dielectric constant solid dielectric transmission lines that intrinsically produce ideal rectangular high voltage pulses when charged and switched into matched impedance loads. Voltage levels may be increased by Marx and/or Blumlein principles incorporating spark gap or, preferentially, solid state switches (such as optically triggered thyristors) which produce reliable, high repetition rate operation. Moreover, these Marxed pulse generators can be DC charged and do not require additional pulse forming circuitry, pulse forming lines, transformers, or an a high voltage spark gap output switch. The apparatus accommodates a wide range of voltages, impedances, pulse durations, pulse repetition rates, and duty cycles. The resulting mobile or flight platform friendly cylindrical geometric configuration is much more compact, light-weight, and robust than conventional linear geometries, or pulse generators constructed from conventional components. Installing additional circuitry may accommodate optional pulse shape improvements. The Coiled Transmission Lines can also be connected in parallel to decrease the impedance, or in series to increase the pulse length.

The Second Flight of the Sunrise Balloon-borne Solar Observatory: Overview of Instrument Updates, the Flight, the Data, and First Results

Energy Technology Data Exchange (ETDEWEB)

Solanki, S. K.; Riethmüller, T. L.; Barthol, P.; Danilovic, S.; Deutsch, W.; Doerr, H.-P.; Feller, A.; Gandorfer, A.; Germerott, D.; Gizon, L.; Grauf, B.; Heerlein, K.; Hirzberger, J.; Kolleck, M.; Lagg, A.; Meller, R.; Tomasch, G.; Noort, M. van [Max Planck Institute for Solar System Research, Justus-von-Liebig-Weg 3, D-37077 Göttingen (Germany); Rodríguez, J. Blanco; Blesa, J. L. Gasent, E-mail: solanki@mps.mpg.de [Grupo de Astronomía y Ciencias del Espacio, Universidad de Valencia, E-46980 Paterna, Valencia (Spain); and others

2017-03-01

The Sunrise balloon-borne solar observatory, consisting of a 1 m aperture telescope that provides a stabilized image to a UV filter imager and an imaging vector polarimeter, carried out its second science flight in 2013 June. It provided observations of parts of active regions at high spatial resolution, including the first high-resolution images in the Mg ii k line. The obtained data are of very high quality, with the best UV images reaching the diffraction limit of the telescope at 3000 Å after Multi-Frame Blind Deconvolution reconstruction accounting for phase-diversity information. Here a brief update is given of the instruments and the data reduction techniques, which includes an inversion of the polarimetric data. Mainly those aspects that evolved compared with the first flight are described. A tabular overview of the observations is given. In addition, an example time series of a part of the emerging active region NOAA AR 11768 observed relatively close to disk center is described and discussed in some detail. The observations cover the pores in the trailing polarity of the active region, as well as the polarity inversion line where flux emergence was ongoing and a small flare-like brightening occurred in the course of the time series. The pores are found to contain magnetic field strengths ranging up to 2500 G, and while large pores are clearly darker and cooler than the quiet Sun in all layers of the photosphere, the temperature and brightness of small pores approach or even exceed those of the quiet Sun in the upper photosphere.

Perseus Post-flight

Science.gov (United States)

1991-01-01

Crew members check out the Perseus proof-of-concept vehicle on Rogers Dry Lake, adjacent to the Dryden Flight Research Center, Edwards, California, after a test flight in 1991. Perseus B is a remotely piloted aircraft developed as a design-performance testbed under NASA's Environmental Research Aircraft and Sensor Technology (ERAST) project. Perseus is one of several flight vehicles involved in the ERAST project. A piston engine, propeller-powered aircraft, Perseus was designed and built by Aurora Flight Sciences Corporation, Manassas, Virginia. The objectives of Perseus B's ERAST flight tests have been to reach and maintain horizontal flight above altitudes of 60,000 feet and demonstrate the capability to fly missions lasting from 8 to 24 hours, depending on payload and altitude requirements. The Perseus B aircraft established an unofficial altitude record for a single-engine, propeller-driven, remotely piloted aircraft on June 27, 1998. It reached an altitude of 60,280 feet. In 1999, several modifications were made to the Perseus aircraft including engine, avionics, and flight-control-system improvements. These improvements were evaluated in a series of operational readiness and test missions at the Dryden Flight Research Center, Edwards, California. Perseus is a high-wing monoplane with a conventional tail design. Its narrow, straight, high-aspect-ratio wing is mounted atop the fuselage. The aircraft is pusher-designed with the propeller mounted in the rear. This design allows for interchangeable scientific-instrument payloads to be placed in the forward fuselage. The design also allows for unobstructed airflow to the sensors and other devices mounted in the payload compartment. The Perseus B that underwent test and development in 1999 was the third generation of the Perseus design, which began with the Perseus Proof-Of-Concept aircraft. Perseus was initially developed as part of NASA's Small High-Altitude Science Aircraft (SHASA) program, which later evolved

Wind and Wake Sensing with UAV Formation Flight: System Development and Flight Testing

Science.gov (United States)

Larrabee, Trenton Jameson

Wind turbulence including atmospheric turbulence and wake turbulence have been widely investigated; however, only recently it become possible to use Unmanned Aerial Vehicles (UAVs) as a validation tool for research in this area. Wind can be a major contributing factor of adverse weather for aircraft. More importantly, it is an even greater risk towards UAVs because of their small size and weight. Being able to estimate wind fields and gusts can potentially provide substantial benefits for both unmanned and manned aviation. Possible applications include gust suppression for improving handling qualities, a better warning system for high wind encounters, and enhanced control for small UAVs during flight. On the other hand, the existence of wind can be advantageous since it can lead to fuel savings and longer duration flights through dynamic soaring or thermal soaring. Wakes are an effect of the lift distribution across an aircraft's wing or tail. Wakes can cause substantial disturbances when multiple aircraft are moving through the same airspace. In fact, the perils from an aircraft flying through the wake of another aircraft is a leading cause of the delay between takeoff times at airports. Similar to wind, though, wakes can be useful for energy harvesting and increasing an aircraft's endurance when flying in formation which can be a great advantage to UAVs because they are often limited in flight time due to small payload capacity. Formation flight can most often be seen in manned aircraft but can be adopted for use with unmanned systems. Autonomous flight is needed for flying in the "sweet spot" of the generated wakes for energy harvesting as well as for thermal soaring during long duration flights. For the research presented here formation flight was implemented for the study of wake sensing and gust alleviation. The major contributions of this research are in the areas of a novel technique to estimate wind using an Unscented Kalman filter and experimental wake

Seks on parem kui Pelevin / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

2011-01-01

Tutvustus: Pelevin, Viktor. Libalooma Püha Raamat / tõlkinud Maiga Varik. Tallinn : Varrak, 2011 ; Weber, Andreas. Kõik me tunneme / tõlkinud Krista Räni. Tallinn : Varrak, 2011 ; Vella, Juri. Järvetuul / tõlkinud Art Leete. Tallinn : Varrak, 2011

Kirjanduskriitikute suvemängud / Kärt Hellerma

Index Scriptorium Estoniae

Hellerma, Kärt, 1956-

2007-01-01

Arvustus: Lodge, David. Ühest kohast teise / tlk. Aet Varik. Tallinn : Varrak, 2005 ; Lodge, David. Väike maailm / tlk. Kersti Unt. Tallinn : Varrak, 1996 ; Lodge, David. Väärt töö / tlk. Kersti Unt. Tallinn : Varrak, 2006

Uusi raamatuid / Lauri Eesmaa

Index Scriptorium Estoniae

Eesmaa, Lauri

2011-01-01

Tutvustus: Dante Alighieri. Jumalik komöödia : Põrgu. Tallinn : Eesti Keele Sihtasutus, 2011. Perec, Georges. Ruumiliigid. Tallinn : Kultuurileht, 2011. Kadare, Ismail. Kuri aasta / albaania keelest tõlkinud Kalle Kasemaa. Tallinn : Kultuurileht, 2011 (Loomingu Raamatukogu ; 17-18/2011)

Õdusad Inglise lastelood / Triin Tael

Index Scriptorium Estoniae

Tael, Triin

2008-01-01

Tutvustus: Potter, Beatrix. Lugu Benjamin Nudisabast. Tallinn : Ilo, c2008 ; Potter, Beatrix. Lugu Orav Käbikäpast. Tallinn : Ilo, c2008 ; Potter, Beatrix. Lugu Peeter Pikk-Kõrvast. Tallinn : Ilo, c2008. Ka Astrid Lindgrenist ja tema raamatutest

Viiv: sügis 1963-1973 : Viivi Luige luule jaapanlikkus / Külliki Kuusk

Index Scriptorium Estoniae

Kuusk, Külliki, 1975-

2007-01-01

Viivi Luige luulekogude "Taevaste tuul" (Tallinn : Eesti Raamat, 1966), "Lauludemüüja" (Tallinn : Eesti Raamat, 1968) ja "Hääl" (Tallinn : Perioodika, 1968) poeetikast. Uku Masingu ja Viivi Luige seotusest, jaapani luule mõjudest Viivi Luige loomingule

X-43A Flight Controls

Science.gov (United States)

Baumann, Ethan

2006-01-01

A viewgraph presentation detailing X-43A Flight controls at NASA Dryden Flight Research Center is shown. The topics include: 1) NASA Dryden, Overview and current and recent flight test programs; 2) Unmanned Aerial Vehicle Synthetic Aperture Radar (UAVSAR) Program, Program Overview and Platform Precision Autopilot; and 3) Hyper-X Program, Program Overview, X-43A Flight Controls and Flight Results.

F-16XL ship #1 (#849) during first flight of the Digital Flight Control System (DFCS)

Science.gov (United States)

1997-01-01

After completing its first flight with the Digital Flight Control System on December 16, 1997, the F-16XL #1 aircraft began a series of envelope expansion flights. On January 27 and 29, 1998, it successfully completed structural clearance tests, as well as most of the load testing Only flights at Mach 1.05 at 10,000 feet, Mach 1.1 at 15,000 feet, and Mach 1.2 at 20,000 feet remained. During the next flight, on February 4, an instrumentation problem cut short the planned envelope expansion tests. After the problem was corrected, the F-16XL returned to flight status, and on February 18 and 20, flight control and evaluation flights were made. Two more research flights were planned for the following week, but another problem appeared. During the ground start up, project personnel noticed that the leading edge flap moved without being commanded. The Digital Flight Control Computer was sent to the Lockheed-Martin facility at Fort Worth, where the problem was traced to a defective chip in the computer. After it was replaced, the F-16XL #1 flew a highly successful flight controls and handling qualities evaluation flight on March 26, clearing the way for the final tests. The final limited loads expansion flight occurred on March 31, and was fully successful. As a result, the on-site Lockheed-Martin loads engineer cleared the aircraft to Mach 1.8. The remaining two handling qualities and flight control evaluation flights were both made on April 3, 1998. These three flights concluded the flight test portion of the DFCS upgrade.

DAST in Flight

Science.gov (United States)

1980-01-01

The modified BQM-34 Firebee II drone with Aeroelastic Research Wing (ARW-1), a supercritical airfoil, during a 1980 research flight. The remotely-piloted vehicle, which was air launched from NASA's NB-52B mothership, participated in the Drones for Aerodynamic and Structural Testing (DAST) program which ran from 1977 to 1983. The DAST 1 aircraft (Serial #72-1557), pictured, crashed on 12 June 1980 after its right wing ripped off during a test flight near Cuddeback Dry Lake, California. The crash occurred on the modified drone's third free flight. These are the image contact sheets for each image resolution of the NASA Dryden Drones for Aerodynamic and Structural Testing (DAST) Photo Gallery. From 1977 to 1983, the Dryden Flight Research Center, Edwards, California, (under two different names) conducted the DAST Program as a high-risk flight experiment using a ground-controlled, pilotless aircraft. Described by NASA engineers as a 'wind tunnel in the sky,' the DAST was a specially modified Teledyne-Ryan BQM-34E/F Firebee II supersonic target drone that was flown to validate theoretical predictions under actual flight conditions in a joint project with the Langley Research Center, Hampton, Virginia. The DAST Program merged advances in electronic remote control systems with advances in airplane design. Drones (remotely controlled, missile-like vehicles initially developed to serve as gunnery targets) had been deployed successfully during the Vietnamese conflict as reconnaissance aircraft. After the war, the energy crisis of the 1970s led NASA to seek new ways to cut fuel use and improve airplane efficiency. The DAST Program's drones provided an economical, fuel-conscious method for conducting in-flight experiments from a remote ground site. DAST explored the technology required to build wing structures with less than normal stiffness. This was done because stiffness requires structural weight but ensures freedom from flutter-an uncontrolled, divergent oscillation of

Venemaa lähiajalugu : hajamõtteid uuematest tõlkeraamatutest / Tõnu Tannberg

Index Scriptorium Estoniae

Tannberg, Tõnu, 1961-

2000-01-01

Arvustus: Radzinski, Edvard. Stalin. Tallinn : Varrak, 2000 ; Rubin, Nikolai. Lavrenti Beria : müüt ja reaalsus. Tallinn : Olion, 2000 ; Sudoplatov, Pavel. Erioperatsioonid : Ljubjanka ja Kreml 1930-1950. Tallinn : Olion, 2000. Ka venekeelse ajalookirjanduse eestindamisel üldiselt esinevatest probleemidest

Fantacy't erinevale maitsele / Sash Uusjärv

Index Scriptorium Estoniae

Uusjärv, Sash

2011-01-01

Arvustus: Westerfeld, Scott. Inetud / inglise keelest tõlkinud Maali Käbin. Tallinn : Varrak, 2011; Flinn, Alex. Koletu / inglise keelest tõlkinud Kret Kaasik. Tallinn : Varrak, 2010 ; Banner, Catherine. Kuninga silmad / inglise keelest tõlkinud Tanel Rõigas. Tallinn : Varrak, 2011

Flapping wing flight can save aerodynamic power compared to steady flight.

Science.gov (United States)

Pesavento, Umberto; Wang, Z Jane

2009-09-11

Flapping flight is more maneuverable than steady flight. It is debated whether this advantage is necessarily accompanied by a trade-off in the flight efficiency. Here we ask if any flapping motion exists that is aerodynamically more efficient than the optimal steady motion. We solve the Navier-Stokes equation governing the fluid dynamics around a 2D flapping wing, and determine the minimal aerodynamic power needed to support a specified weight. While most flapping wing motions are more costly than the optimal steady wing motion, we find that optimized flapping wing motions can save up to 27% of the aerodynamic power required by the optimal steady flight. We explain the cause of this energetic advantage.

Flight code validation simulator

Science.gov (United States)

Sims, Brent A.

1996-05-01

An End-To-End Simulation capability for software development and validation of missile flight software on the actual embedded computer has been developed utilizing a 486 PC, i860 DSP coprocessor, embedded flight computer and custom dual port memory interface hardware. This system allows real-time interrupt driven embedded flight software development and checkout. The flight software runs in a Sandia Digital Airborne Computer and reads and writes actual hardware sensor locations in which Inertial Measurement Unit data resides. The simulator provides six degree of freedom real-time dynamic simulation, accurate real-time discrete sensor data and acts on commands and discretes from the flight computer. This system was utilized in the development and validation of the successful premier flight of the Digital Miniature Attitude Reference System in January of 1995 at the White Sands Missile Range on a two stage attitude controlled sounding rocket.

Lastevihkaja Daniil Harms ja puuslik Leonid Iljitš Brežnev / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

2011-01-01

Tutvustus: Harms, Daniil. Väljapudunevad vanaeided / tõlkinud Ilona Martson ja Rein Saluri. Tallinn : Tänapäev, 2011 ; Bourget, Paul. Õpilane / tõlkinud Kattri Ezzoubi. Tallinn : Eesti Raamat, 2011 ; Mletšin, Leonid. Brežnev. Tallinn : Varrak, 2011

Hasso Krulli eepiline pesamuna / Rein Veidemann

Index Scriptorium Estoniae

Veidemann, Rein, 1946-

2015-01-01

Eesti Kultuurkapitali aastapreemia laureaat Hasso Krull. Arvustus: Krull, Hasso. Pesa : tekstid 2000-2012. Tallinn : Eesti Keele Sihtasutus, 2014 ; Krull, Hasso. Muna : tekstid 1987-2012. Tallinn : Eesti Keele Sihtasutus, 2014 ; Krull, Hasso. Kui kivid olid veel pehmed. Tallinn : Eesti Keele Sihtasutus, 2014

Four vision of contemporary Estonian art : the series of exhibitions Estonian art / Heie Treier

Index Scriptorium Estoniae

Treier, Heie, 1963-

2000-01-01

Neljast eesti kunsti näitusest 2000. a. märtsis-aprillis Tartus ja Tallinnas, nende kuraatoritest: Toomas Vint, Reet Varblane, Peeter Allik, Johannes Saar. Déj́-vu (Tallinn). Naturalism (Tallinn). AIDS kultuuris (Tallinn). Eneseksjäämine (Tartu)

Design, construction, characterization, and use of a detector to measure time of flight of cosmic rays

Science.gov (United States)

Araujo, A. C.; Felix, J.

2017-01-01

In the study of cosmic rays, measurements of time of flight and momentum have been used to identify incident particles from its physical properties, like mass. In this document we present the design, construction, characterization, and operation of a detector to measure time of flight of cosmic rays. The device is comprised of three small plates of plastic scintillator arranged in vertical straight line, coupled to one photomultiplier tube. The analogical output has been connected to a data acquisition system to obtain the number of digital pulses per millisecond. We present details of design, construction, operation, and preliminary results.

A real-time expert system for self-repairing flight control

Science.gov (United States)

Gaither, S. A.; Agarwal, A. K.; Shah, S. C.; Duke, E. L.

1989-01-01

An integrated environment for specifying, prototyping, and implementing a self-repairing flight-control (SRFC) strategy is described. At an interactive workstation, the user can select paradigms such as rule-based expert systems, state-transition diagrams, and signal-flow graphs and hierarchically nest them, assign timing and priority attributes, establish blackboard-type communication, and specify concurrent execution on single or multiple processors. High-fidelity nonlinear simulations of aircraft and SRFC systems can be performed off-line, with the possibility of changing SRFC rules, inference strategies, and other heuristics to correct for control deficiencies. Finally, the off-line-generated SRFC can be transformed into highly optimized application-specific real-time C-language code. An application of this environment to the design of aircraft fault detection, isolation, and accommodation algorithms is presented in detail.

Perseus in Flight

Science.gov (United States)

1991-01-01

The Perseus proof-of-concept vehicle flies over Rogers Dry Lake at the Dryden Flight Research Center, Edwards, California, to test basic design concepts for the remotely-piloted, high-altitude vehicle. Perseus B is a remotely piloted aircraft developed as a design-performance testbed under NASA's Environmental Research Aircraft and Sensor Technology (ERAST) project. Perseus is one of several flight vehicles involved in the ERAST project. A piston engine, propeller-powered aircraft, Perseus was designed and built by Aurora Flight Sciences Corporation, Manassas, Virginia. The objectives of Perseus B's ERAST flight tests have been to reach and maintain horizontal flight above altitudes of 60,000 feet and demonstrate the capability to fly missions lasting from 8 to 24 hours, depending on payload and altitude requirements. The Perseus B aircraft established an unofficial altitude record for a single-engine, propeller-driven, remotely piloted aircraft on June 27, 1998. It reached an altitude of 60,280 feet. In 1999, several modifications were made to the Perseus aircraft including engine, avionics, and flight-control-system improvements. These improvements were evaluated in a series of operational readiness and test missions at the Dryden Flight Research Center, Edwards, California. Perseus is a high-wing monoplane with a conventional tail design. Its narrow, straight, high-aspect-ratio wing is mounted atop the fuselage. The aircraft is pusher-designed with the propeller mounted in the rear. This design allows for interchangeable scientific-instrument payloads to be placed in the forward fuselage. The design also allows for unobstructed airflow to the sensors and other devices mounted in the payload compartment. The Perseus B that underwent test and development in 1999 was the third generation of the Perseus design, which began with the Perseus Proof-Of-Concept aircraft. Perseus was initially developed as part of NASA's Small High-Altitude Science Aircraft (SHASA

Characterizing Scintillator Response with Neutron Time-of-Flight

Science.gov (United States)

Palmisano, Kevin; Visca, Hannah; Caves, Louis; Wilkinson, Corey; McClow, Hannah; Padalino, Stephen; Forrest, Chad; Katz, Joe; Sangster, Craig; Regan, Sean

2017-10-01

Neutron scintillator diagnostics for ICF can be characterized using the neutron time-of-flight (nTOF) line on Geneseo's 1.7 MV Tandem Pelletron Accelerator. Neutron signals can be differentiated from gamma signals by employing a coincidence method called the associated particle technique (APT). In this measurement, a 2.1 MeV beam of deuterons incident on a deuterated polyethylene target produces neutrons via the d(d,n)3He reaction. A BC-412 plastic scintillator, placed at a scattering angle of 152º, detects 1.76 MeV neutrons in coincidence with the 2.56 MeV 3He ions at an associated angle of 10º. The APT is used to identify the 1.76 MeV neutron while the nTOF line determines its energy. By gating only mono-energetic neutrons, the instrument response function of the scintillator can be determined free from background scattered neutrons and gamma rays. Funded in part by a Grant from the DOE, through the Laboratory for Laser Energetics.

Orion Exploration Flight Test Post-Flight Inspection and Analysis

Science.gov (United States)

Miller, J. E.; Berger, E. L.; Bohl, W. E.; Christiansen, E. L.; Davis, B. A.; Deighton, K. D.; Enriquez, P. A.; Garcia, M. A.; Hyde, J. L.; Oliveras, O. M.

2017-01-01

The principal mechanism for developing orbital debris environment models, is to make observations of larger pieces of debris in the range of several centimeters and greater using radar and optical techniques. For particles that are smaller than this threshold, breakup and migration models of particles to returned surfaces in lower orbit are relied upon to quantify the flux. This reliance on models to derive spatial densities of particles that are of critical importance to spacecraft make the unique nature of the EFT-1's return surface a valuable metric. To this end detailed post-flight inspections have been performed of the returned EFT-1 backshell, and the inspections identified six candidate impact sites that were not present during the pre-flight inspections. This paper describes the post-flight analysis efforts to characterize the EFT-1 mission craters. This effort included ground based testing to understand small particle impact craters in the thermal protection material, the pre- and post-flight inspection, the crater analysis using optical, X-ray computed tomography (CT) and scanning electron microscope (SEM) techniques, and numerical simulations.

Capital Flight and Economic Performance

OpenAIRE

Beja, Edsel Jr.

2007-01-01

Capital flight aggravates resource constraints and contributes to undermine long-term economic growth. Counterfactual calculations on the Philippines suggest that capital flight contributed to lower the quality of long-term economic growth. Sustained capital flight over three decades means that capital flight had a role for the Philippines to lose the opportunities to achieve economic takeoff. Unless decisive policy actions are taken up to address enduring capital flight and manage the macroe...

Recent estimates of capital flight

OpenAIRE

Claessens, Stijn; Naude, David

1993-01-01

Researchers and policymakers have in recent years paid considerable attention to the phenomenon of capital flight. Researchers have focused on four questions: What concept should be used to measure capital flight? What figure for capital flight will emerge, using this measure? Can the occurrence and magnitude of capital flight be explained by certain (economic) variables? What policy changes can be useful to reverse capital flight? The authors focus strictly on presenting estimates of capital...

Parandada püksipõlve augu väljalõikamise teel / Jaak Tomberg

Index Scriptorium Estoniae

Tomberg, Jaak, 1980-

2010-01-01

Arvustus: Saar, Anti. Kuidas sa ära läksid ja mina maha jäin : [jutud]. Tallinn : Eesti Keele Sihtasutus, 2006 ; Saar, Anti. Nemad kaks : [lühiromaan]. Tallinn : Eesti Keele Sihtasutus, 2008 ; Tekste siledast ruumist : [jutud]. Tallinn : Eesti Keele Sihtasutus, 2009

Nii, nagu oli, seal, kus oli / Heili Sibrits

Index Scriptorium Estoniae

Sibrits, Heili, 1977-

2010-01-01

Arvustus: Goodwin, Jason. Janitšaride puu : [romaan] / inglise keelest tõlkinud Juhan Habicht. Tallinn : Varrak, 2006 ; Goodwin, Jason. Maokivi : [kriminaalromaan] / inglise keelest tõlkinud Juhan Habicht. Tallinn : Varrak, 2008 ; Goodwin, Jason. Bellini kaart / inglise keelest tõlkinud Juhan Habicht. Tallinn : Varrak, 2010

Pilk uuele "Põhjamaade romaani" sarjale / Hilve Rebane

Index Scriptorium Estoniae

Rebane, Hilve, 1938-2012

1999-01-01

Bengtson, Frans G. Orm Punane / tlk. Anu Saluäär. Tallinn : Eesti Raamat, 1997 ; Wassmo, Herbjırg. Dina raamat / tlk. Elvi Lumet. Tallinn : Eesti Raamat, 1997 ; Tunström, Göran. Varas / tlk. Ene Mäe. Tallinn : Eesti Raamat, 1999

Surnud mehe käsi / Veiko Belials

Index Scriptorium Estoniae

Belials, Veiko, 1966-

1997-01-01

Arvustus: Asimov, Isaac. Asum / inglise k. tlk. Linda Ariva. Tallinn : Eesti Raamat, 1985. (Mirabilia); Asimov, Isaac. Asum ja impeerium / inglise k. tlk. Linda Ariva. Tallinn : Eesti Raamat, 1989. (Mirabilia); Asimov, Isaac. Teine asum / inglise k. tlk. Indrek Elling. Tallinn : Eesti Raamat, 1996. (Mirabilia)

Telliskivist Peeter Suureni / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

2005-01-01

Tutvustus: Fowles, John. Daniel Martin / inglise keelest tõlkinud Viktoria Traat. Tallinn : Varrak, 2005 ; Undset, Sigrid. Põlev põõsas / norra keelest tõlkinud Elvi Lumet. Tallinn : Eesti Raamat, 2005 ; Hughes, Lindsey. Peeter Suur / inglise keelest tõlkinud Lauri Vahtre. Tallinn : Varrak, 2005

Tallinna, Riia ja Helsingi ajaloolised atlased / Tõnis Liibek

Index Scriptorium Estoniae

Liibek, Tõnis, 1976-

2013-01-01

Arvustus: Tallinn ajaloolistel linnaplaanidel 1634-1989 [kaart] = Maps of the City of Tallinn =Tallinn auf den Stadtplanen = Планы города Таллинна. Tallinn, 2011 ; Margarita Barzdeviča. Rīga zviedru laika kartēs un plānos 1621-1710. Latvijas Vēstures Insitūta Apgāds. Rīga, 2011 ; Helsinki - Helsingfors. Historiallinen kaupunkikartasto - Historic Towns Atlas. Helsinki, 2009

Book reviews / Carolina Pihelgas, Peeter Helme and Jan Kaus

Index Scriptorium Estoniae

Pihelgas, Carolina, 1986-

2016-01-01

Arvustus: Sommer, Lauri. Kunagi: 2008-2015. Räestu [Võrumaa] : Tiivaalune, 2015 ; Rooste, Jürge. Ideaalne abikaasa. Saarde ; Pärnu : [Jumalikud Ilmutused], 2015 ; Ruitlane, Olavi. Vee peal. Tallinn : ZA/UM, 2015 ; Riismaa, Kaur. Pühamägi. Tallinn : Verb, 2015 ; Riismaa, Kaur. Pimeda mehe aiad. Tallinn : Tänapäev, 2015 ; Raud, Rein. Täiusliku lause surm. Tallinn : Mustvalge Kirjastus, 2015 ; Matsin, Paavo. Gogoli disko. Viljandi : Lepp ja Nagel, 2015 ; Lennuk, Urmas. Ükskord Eestimaal. Viljandi : Ugala Teater, 2015

The relationship of certified flight instructors' emotional intelligence levels on flight student advancement

Science.gov (United States)

Hokeness, Mark Merrill

Aviation researchers estimate airline companies will require nearly 500,000 pilots in the next 20 years. The role of a Certified Flight Instructor (CFI) is to move student pilots to professional pilots with training typically conducted in one-on-one student and instructor sessions. The knowledge of aviation, professionalism as a teacher, and the CFI’s interpersonal skills can directly affect the successes and advancement of a student pilot. A new and emerging assessment of people skills is known as emotional intelligence (EI). The EI of the CFI can and will affect a flight students’ learning experiences. With knowledge of emotional intelligence and its effect on flight training, student pilot dropouts from aviation may be reduced, thus helping to ensure an adequate supply of pilots. Without pilots, the growth of the commercial aviation industry will be restricted. This mixed method research study established the correlation between a CFI’s measured EI levels and the advancement of flight students. The elements contributing to a CFI’s EI level were not found to be teaching or flight-related experiences, suggesting other life factors are drawn upon by the CFI and are reflected in their emotional intelligence levels presented to flight students. Students respond positively to CFIs with higher levels of emotional intelligence. Awareness of EI skills by both the CFI and flight student contribute to flight student successes and advancement.

Insect flight muscle metabolism

NARCIS (Netherlands)

Horst, D.J. van der; Beenakkers, A.M.Th.; Marrewijk, W.J.A. van

1984-01-01

The flight of an insect is of a very complicated and extremely energy-demanding nature. Wingbeat frequency may differ between various species but values up to 1000 Hz have been measured. Consequently metabolic activity may be very high during flight and the transition from rest to flight is

Secondary beam line phase space measurement and modeling at LAMPF

International Nuclear Information System (INIS)

Floyd, R.; Harrison, J.; Macek, R.; Sanders, G.

1979-01-01

Hardware and software have been developed for precision on-line measurement and fitting of secondary beam line phase space parameters. A system consisting of three MWPC planes for measuring particle trajectories, in coincidence with a time-of-flight telescope and a range telescope for particle identification, has been interfaced to a computer. Software has been developed for on-line track reconstruction, application of experimental cuts, and fitting of two-dimensional phase space ellipses for each particle species. The measured distributions have been found to agree well with the predictions of the Monte Carlo program DECAY TURTLE. The fitted phase space ellipses are a useful input to optimization routines, such as TRANSPORT, used to search for superior tunes. Application of this system to the LAMPF Stopped Muon Channel is described

14 CFR 63.23 - Special purpose flight engineer and flight navigator certificates: Operation of U.S.-registered...

Science.gov (United States)

2010-01-01

... purpose flight engineer and flight navigator certificates: Operation of U.S.-registered civil airplanes... flight engineer or flight navigator duties on a civil airplane of U.S. registry, leased to a person not a... certificate holder is performing flight engineer or flight navigator duties on the U.S.-registered civil...

Vadja sõnaraamat kui kunstiteos / Kristiina Ross

Index Scriptorium Estoniae

Ross, Kristiina, 1955-

2011-01-01

Arvustus: Vadja keele sõnaraamat. 1 / toimetanud Elna Adler, Merle Leppik. Tallinn : AE Signalet, 1990 ; Vadja keele sõnaraamat. 2, [K -küüttöseltšä] = Словарь водского языка. 2 / toimetanud Elna Adler, Merle Leppik. [Tallinn] ; [Tallinn] : Teaduste Akadeemia Kirjastus, 1994 ; Vadja keele sõnaraamat. 3, L - müüäG] = Словарь водского языка / toimetanud Elna Adler, Merle Leppik. [Tallinn] ; [Tallinn] : Eesti Keele Instituut, 1996 ; Vadja keele sõnaraamat. 4, [N - P] = Словарь водского языка. 4, [N - P] / toimetanud: Elna Adler, Merle Leppik. [Tallinn] : Eesti Keele Sihtasutus, 2000 ; Vadja keele sõnaraamat. 5, [R-S] = Словарь водского языка. 5, [R-S] / toimetanud Silja Grünberg. Tallinn : Eesti Keele Sihtasutus, 2006 ; Vadja keele sõnaraamat. 6, [Š-T] = Словарь водского языка. 6, [Š-T] / toimetanud Silja Grünberg. Tallinn : Eesti Keele Sihtasutus, 2010 ; Vadja keele sõnaraamat. 7 = Словарь водского языка / toimetanud Silja Grünberg. Tallinn : Eesti Keele Sihtasutus, 2011

14 CFR 23.865 - Fire protection of flight controls, engine mounts, and other flight structure.

Science.gov (United States)

2010-01-01

... 14 Aeronautics and Space 1 2010-01-01 2010-01-01 false Fire protection of flight controls, engine... controls, engine mounts, and other flight structure. Flight controls, engine mounts, and other flight... they are capable of withstanding the effects of a fire. Engine vibration isolators must incorporate...

Head lood halvast ajast / Karl Martin Sinijärv

Index Scriptorium Estoniae

Sinijärv, Karl Martin, 1971-

2003-01-01

Arvustus: Akunin, Boriss. Azazel : romaan / vene keelest tõlkinud Jüri Ojamaa. [Tallinn] : Tänapäev, 2003; Akunin, Boriss. Türgi gambiit : romaan / vene keelest tõlkinud Veronika Einberg. [Tallinn] : Tänapäev, 2003; Akunin, Boriss. Leviathan. Tallinn : Tänapäev, 2003

Elu mütoloogilises psühhoruumis / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

2009-01-01

Tutvustus: Lukjanenko, Sergei. Öine Vahtkond / tlk. Tanel Rõigas. Tallinn : Varrak, 2008 ; Rubina, Dina. Päikeselisel tänavapoolel / tlk. Veronika Einberg. Tallinn : Tänapäev, 2008 ; Suhhotšev, Aleksandr. Goa sündroom / tlk. Veronika Einberg. Tallinn : Tänapäev, 2008

Igal puul oma õunad ehk Kõnekäände mitmel teemal : [uusi raamatuid rahvapärastest ütlustest] / Asta Õim

Index Scriptorium Estoniae

Õim, Asta, 1943-

2002-01-01

Arvustus: Tere, tere, teid ma tunnen ...: Soove, tervitusi, tänamisi / koost. Anne Hussar. Tallinn, 2002 ; Elevant voodi all, voodi lae all : keerdküsimusi loomadest / koost. Piret Voolaid. Tallinn, 2002 ; Mis sa soiud, võta soodat! : Sajatusi, osatusi, parastamisi / koost. Anneli Baran. Tallinn, 2002

B-MINE, the balloon-borne microcalorimeter nuclear line explorer

DEFF Research Database (Denmark)

Silver, E; Schnopper, H; Jones, C

2001-01-01

introduces the concept of focusing optics and microcalorimeter spectroscopy to nuclear line emission astrophysics. B-MINE has a thin, plastic foil telescope multilayered to maximize the reflectivity in a 20 keV band centered at 68 keV and a microcalorimeter array optimized for the same energy band....... This combination provides a reduced background, an energy resolution of 50 eV and a 3sigma sensitivity in 10(6) s of 3.3 x 10(-7) ph cm(-2) s(-1) at 68 keV. During the course of a long duration balloon flight, B-MINE could carry out a detailed study of the Ti-44 emission line centroid and width in CAS A....

B-MINE, the balloon-borne microcalorimeter nuclear line explorer

DEFF Research Database (Denmark)

Silver, E.; Schnopper, H.; Jones, C.

2002-01-01

introduces the concept of focusing optics and microcalorimeter spectroscopy to nuclear line emission astrophysics. B-MINE has a thin, plastic foil telescope multilayered to maximize the reflectivity in a 20 keV band centered at 68 keV and a microcalorimeter array optimized for the same energy band....... This combination provides a reduced background, an energy resolution of 50 eV and a 3σ sensitivity in 106 s of 3.3 × 10-7 ph cm-2 s-1 at 68 keV. During the course of a long duration balloon flight. B-MINE could carry out a detailed study of the 44Ti emission line centroid and width in CASA....

Navigation and flight director guidance for the NASA/FAA helicopter MLS curved approach flight test program

Science.gov (United States)

Phatak, A. V.; Lee, M. G.

1985-01-01

The navigation and flight director guidance systems implemented in the NASA/FAA helicopter microwave landing system (MLS) curved approach flight test program is described. Flight test were conducted at the U.S. Navy's Crows Landing facility, using the NASA Ames UH-lH helicopter equipped with the V/STOLAND avionics system. The purpose of these tests was to investigate the feasibility of flying complex, curved and descending approaches to a landing using MLS flight director guidance. A description of the navigation aids used, the avionics system, cockpit instrumentation and on-board navigation equipment used for the flight test is provided. Three generic reference flight paths were developed and flown during the test. They were as follows: U-Turn, S-turn and Straight-In flight profiles. These profiles and their geometries are described in detail. A 3-cue flight director was implemented on the helicopter. A description of the formulation and implementation of the flight director laws is also presented. Performance data and analysis is presented for one pilot conducting the flight director approaches.

Aviator's Fluid Balance During Military Flight.

Science.gov (United States)

Levkovsky, Anna; Abot-Barkan, Sivan; Chapnik, Leah; Doron, Omer; Levy, Yuval; Heled, Yuval; Gordon, Barak

2018-02-01

A loss of 1% or more of bodyweight due to dehydration has a negative effect on cognitive performance, which could critically affect flight safety. There is no mention in the literature concerning the amounts of military pilots' fluid loss during flight. The aim of this study was to quantify fluid loss of pilots during military flight. There were 48 aviators (mean age 23.9) from the Israeli Air Force who participated in the study, which included 104 training flights in various flight platforms. Bodyweight, urine specific gravity, and environmental heat strain were measured before and after each flight. Fluid loss was calculated as the weight differences before and after the flight. We used a univariate and one-way ANOVA to analyze the effect of different variables on the fluid loss. The mean fluid loss rate was 462 ml · h-1. The results varied among different aircraft platforms and depended on flight duration. Blackhawk pilots lost the highest amount of fluids per flight, albeit had longer flights (mean 108 min compared to 35.5 in fighter jets). Jet fighter pilots had the highest rate of fluid loss per hour of flight (up to 692 ml, extrapolated). Overall, at 11 flights (11%) aircrew completed their flight with a meaningful fluid loss. We conclude that military flights may be associated with significant amount of fluid loss among aircrew.Levkovsky A, Abot-Barkan S, Chapnik L, Doron O, Levy Y, Heled Y, Gordon B. Aviator's fluid balance during military flight. Aerosp Med Hum Perform. 2018; 89(2):9498.

Apollo experience report: Development flight instrumentation. [telemetry equipment for space flight test program

Science.gov (United States)

Farmer, N. B.

1974-01-01

Development flight instrumentation was delivered for 25 Apollo vehicles as Government-furnished equipment. The problems and philosophies of an activity that was concerned with supplying telemetry equipment to a space-flight test program are discussed. Equipment delivery dates, system-design details, and flight-performance information for each mission also are included.

Kolmekordne kupar / Rein Saluri

Index Scriptorium Estoniae

Saluri, Rein

1998-01-01

Arvustus: Kristof, Agota. Kaustik; Katsumus; Kolmas vale / prantsuse k. tlk. Urmas Rattus. Tallinn : Varrak, 1997. (Moodne klassika); Oz, Amos. Ära ütle, et öö / heebrea k. tlk. Kalle Kasemaa. Tallinn : Kupar, 1998; Weldon, Fay. Kuu Minneapolise kohal / inglise k. tlk. Faina Laksberg. Tallinn : Kupar, 1997

Õ, ehk, Loovtöötaja kottimine / Sven =Kivisildnik

Index Scriptorium Estoniae

Kivisildnik, Sven, pseud., 1964-

2001-01-01

Arvustus: Sinijärv, Karl Martin. Towntown & 28 : viies rühm poeese. Tallinn : Varrak, 1999 ; Sinijärv, Karl Martin. Sobimus. Tallinn : Artmiks, 1999 ; Neid vigu me ei korda / Asko Künnap, Jürgen Rooste, Karl Martin Sinijärv. Tallinn : Näo Kirik, 2000

Iharus iseenda järele / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

2006-01-01

Tutvustus: Gide, André. Surra, et elada / tlk. Leena Tomasberg. Tallinn : Varrak, 2006 ; Soosaar, Martti. Lase vareseid! Tallinn : Tänapäev, 2006 ; Otsides : Juhan Peegel. Meenutusi pikalt teelt / koost. Maarja Lõhmus. Tallinn : Tänapäev, 2006 ; Steffenson, Jakob. Meie, ruhnlased. Tartu : A. Tuulberg, 2006

Kiima kroonikad / Ainiki Väljataga

Index Scriptorium Estoniae

Väljataga, Ainiki

1997-01-01

Arvustus: Mirtem, Valev [Luhaäär, Ingvar]. Valge õis sinisel. S.l., 1996; Mirtem, Valev [Luhaäär, Ingvar]. Loire. Tallinn, 1996; Mirtem, Valev [Luhaäär, Ingvar]. Klaasist lepatriinu. Tallinn, 1996; Mirtem, Valev [Luhaäär, Ingvar]. Toomingais ja sireleis. Tallinn, 1996

Maurice Car̊me'i lihtsad laulud lastele / Helle Michelson

Index Scriptorium Estoniae

Michelson, Helle, 1929-

2003-01-01

Car̊me, Maurice. Muinasjutud Caprine'ile / tõlkinud Helle Michelson. [Tallinn] : Tiritamm, 2002 ; Car̊me, Maurice. Naeruhull kirsipuu : [luuletused] / prantsuse keelest tõlkinud Helvi Jürisson. [Tallinn] : Tiritamm, 2002 ; Car̊me, Maurice. Margareetapäev : [jutustused] / tõlkinud Helle Michelson. [Tallinn] : Varrak, 2000

Flight Tasks and Metrics to Evaluate Laser Eye Protection in Flight Simulators

Science.gov (United States)

2017-07-07

IFR ) IFR Instrument Flight Rules LED Light Emitting Diode LEP Laser Eye Protection MAPP Model Assessing Pilot Performance OD Optical Density...LEP and then use them to assess the impact of wearing LEP in a flight simulator environment. 2 Pending Distribution, A: Approved for public...2005). LEP has the potential to alter distinct characteristics of the visual environment, giving rise to concerns over the impact on flight tasks and

Point Cloud Analysis for Uav-Borne Laser Scanning with Horizontally and Vertically Oriented Line Scanners - Concept and First Results

Science.gov (United States)

Weinmann, M.; Müller, M. S.; Hillemann, M.; Reydel, N.; Hinz, S.; Jutzi, B.

2017-08-01

In this paper, we focus on UAV-borne laser scanning with the objective of densely sampling object surfaces in the local surrounding of the UAV. In this regard, using a line scanner which scans along the vertical direction and perpendicular to the flight direction results in a point cloud with low point density if the UAV moves fast. Using a line scanner which scans along the horizontal direction only delivers data corresponding to the altitude of the UAV and thus a low scene coverage. For these reasons, we present a concept and a system for UAV-borne laser scanning using multiple line scanners. Our system consists of a quadcopter equipped with horizontally and vertically oriented line scanners. We demonstrate the capabilities of our system by presenting first results obtained for a flight within an outdoor scene. Thereby, we use a downsampling of the original point cloud and different neighborhood types to extract fundamental geometric features which in turn can be used for scene interpretation with respect to linear, planar or volumetric structures.

IceBridge Mission Flight Reports

Data.gov (United States)

National Aeronautics and Space Administration — The IceBridge Mission Flight Reports data set contains flight reports from NASA Operation IceBridge Greenland, Arctic, Antarctic, and Alaska missions. Flight reports...

In-flight calibration of the ISGRI camera

International Nuclear Information System (INIS)

Terrier, R.; Lebrun, F.; Belanger, G.; Blondel, C.; David, P.; Goldoni, P.; Goldwurm, A.; Gros, A.; Laurent, P.; Malaguti, G.; Sauvageon, A.; Bazzano, A.; Ubertini, P.; Segreto, A.; Malaguti, G.; Bird, A.J.

2003-01-01

ISGRI, the IBIS low energy camera (15 keV-1 MeV) on board INTEGRAL, is the first large CdTe gamma-ray imager in orbit. We present here an overview of the ISGRI in-flight calibrations performed during the first months after launch. We discuss the stability of the camera as well as the CdTe pixels response under cosmic radiation. The energy calibrations were done using lead and tungsten fluorescence lines and the 22 Na calibration unit. Thermal effects and charge correction algorithm are discussed, and the resulting energy resolution is presented. The ISGRI background spatial and spectral non-uniformity is also described, and some image correction results are presented. ISGRI, despite a few unexpected features like zero rise time events, performs well with only 4,5% noisy or disabled pixels. Thermal effects are at the origin of the largest difference between ground and in-flight data. Correcting for these effects yields good spectral performances close to the expectations with 8.4% at 59.3 keV and 4.9% at 511 keV. The resolution in the high energy band is broader than before launch because of residual rise time gains uncertainties. Handling of these errors requires a larger amount of calibration data than what is available today

X-ray line coincidence photopumping in a solar flare

Science.gov (United States)

Keenan, F. P.; Poppenhaeger, K.; Mathioudakis, M.; Rose, S. J.; Flowerdew, J.; Hynes, D.; Christian, D. J.; Nilsen, J.; Johnson, W. R.

2018-03-01

Line coincidence photopumping is a process where the electrons of an atomic or molecular species are radiatively excited through the absorption of line emission from another species at a coincident wavelength. There are many instances of line coincidence photopumping in astrophysical sources at optical and ultraviolet wavelengths, with the most famous example being Bowen fluorescence (pumping of O III 303.80 Å by He II), but none to our knowledge in X-rays. However, here we report on a scheme where a He-like line of Ne IX at 11.000 Å is photopumped by He-like Na X at 11.003 Å, which predicts significant intensity enhancement in the Ne IX 82.76 Å transition under physical conditions found in solar flare plasmas. A comparison of our theoretical models with published X-ray observations of a solar flare obtained during a rocket flight provides evidence for line enhancement, with the measured degree of enhancement being consistent with that expected from theory, a truly surprising result. Observations of this enhancement during flares on stars other than the Sun would provide a powerful new diagnostic tool for determining the sizes of flare loops in these distant, spatially unresolved, astronomical sources.

Integrated flight path planning system and flight control system for unmanned helicopters.

Science.gov (United States)

Jan, Shau Shiun; Lin, Yu Hsiang

2011-01-01

This paper focuses on the design of an integrated navigation and guidance system for unmanned helicopters. The integrated navigation system comprises two systems: the Flight Path Planning System (FPPS) and the Flight Control System (FCS). The FPPS finds the shortest flight path by the A-Star (A*) algorithm in an adaptive manner for different flight conditions, and the FPPS can add a forbidden zone to stop the unmanned helicopter from crossing over into dangerous areas. In this paper, the FPPS computation time is reduced by the multi-resolution scheme, and the flight path quality is improved by the path smoothing methods. Meanwhile, the FCS includes the fuzzy inference systems (FISs) based on the fuzzy logic. By using expert knowledge and experience to train the FIS, the controller can operate the unmanned helicopter without dynamic models. The integrated system of the FPPS and the FCS is aimed at providing navigation and guidance to the mission destination and it is implemented by coupling the flight simulation software, X-Plane, and the computing software, MATLAB. Simulations are performed and shown in real time three-dimensional animations. Finally, the integrated system is demonstrated to work successfully in controlling the unmanned helicopter to operate in various terrains of a digital elevation model (DEM).

Integrated Flight Path Planning System and Flight Control System for Unmanned Helicopters

Science.gov (United States)

Jan, Shau Shiun; Lin, Yu Hsiang

2011-01-01

This paper focuses on the design of an integrated navigation and guidance system for unmanned helicopters. The integrated navigation system comprises two systems: the Flight Path Planning System (FPPS) and the Flight Control System (FCS). The FPPS finds the shortest flight path by the A-Star (A*) algorithm in an adaptive manner for different flight conditions, and the FPPS can add a forbidden zone to stop the unmanned helicopter from crossing over into dangerous areas. In this paper, the FPPS computation time is reduced by the multi-resolution scheme, and the flight path quality is improved by the path smoothing methods. Meanwhile, the FCS includes the fuzzy inference systems (FISs) based on the fuzzy logic. By using expert knowledge and experience to train the FIS, the controller can operate the unmanned helicopter without dynamic models. The integrated system of the FPPS and the FCS is aimed at providing navigation and guidance to the mission destination and it is implemented by coupling the flight simulation software, X-Plane, and the computing software, MATLAB. Simulations are performed and shown in real time three-dimensional animations. Finally, the integrated system is demonstrated to work successfully in controlling the unmanned helicopter to operate in various terrains of a digital elevation model (DEM). PMID:22164029

Eclipse takeoff and flight

Science.gov (United States)

1998-01-01

This 25-second clip shows the QF-106 'Delta Dart' tethered to the USAF C-141A during takeoff and in flight. NASA Dryden Flight Research Center, Edwards, California, supported a Kelly Space and Technology, Inc. (KST)/U.S. Air Force project known as Eclipse, which demonstrated a reusable tow launch vehicle concept. The purpose of the project was to demonstrate a reusable tow launch vehicle concept that had been conceived and patented by KST. Kelly Space obtained a contract with the USAF Research Laboratory for the tow launch demonstration project under the Small Business Innovation Research (SBIR) program. The USAF SBIR contract included the modifications to turn the QF-106 into the Experimental Demonstrator #1 (EXD-01), and the C141A aircraft to incorporate the tow provisions to link the two aircraft, as well as conducting flight tests. The demonstration consisted of ground and flight tests. These tests included a Combined Systems Test of both airplanes joined by a tow rope, a towed taxi test, and six towed flights. The primary goal of the project was demonstrating the tow phase of the Eclipse concept using a scaled-down tow aircraft (C-141A) and a representative aerodynamically-shaped aircraft (QF-106A) as a launch vehicle. This was successfully accomplished. On December 20, 1997, NASA research pilot Mark Stucky flew a QF-106 on the first towed flight behind an Air Force C-141 in the joint Eclipse project with KST to demonstrate the reusable tow launch vehicle concept developed by KST. Kelly hoped to use the data from the tow tests to validate a tow-to-launch procedure for reusable space launch vehicles. Stucky flew six successful tow tests between December 1997 and February 6, 1998. On February 6, 1998, the sixth and final towed flight brought the project to a successful completion. Preliminary flight results determined that the handling qualities of the QF-106 on tow were very stable; actual flight measured values of tow rope tension were well within predictions

Kolm põnevat raamatut / Kristiina Ehin

Index Scriptorium Estoniae

Ehin, Kristiina, 1977-

2003-01-01

Coelho, Paulo. Palverännak: maagi päevik : [romaan] / tõlkinud Kadre Vaik, Tiina Ristimets. [Tallinn] : Philos, 2002 ; Lescuyer, Jean ; Benchelah, Mehdi. Palverännak Jeruusalemma / prantsuse keelest tõlkinud Jaanus Õunpuu. Tallinn : Olion, 2001 ; Kureishi, Hanif. Lähedus : [romaan] / tõlkinud Aet Varik. [Tallinn] : Huma, 2002

Sugumürsust kirjanikuks

Index Scriptorium Estoniae

2003-01-01

EE kirjanduslabor võrdleb viimase aja kõmukirjanike teoseid: Verrev, Toomas. Margot : (pildikesi päälinna intelligendi elust) : [romaan. Tallinn] : Kadikas, 2003 ; Espenberg, Urmas. Tequila pööripäev: [romaan]. Tallinn : [Agitaator], 2002-2003 ; Aimre, Keith. Ilus Babyss, ehk, Seitse ja pool : [romaan]. Tallinn : Kentaur, 2003.

Eesti meesluule argipäev / Mart Velsker

Index Scriptorium Estoniae

Velsker, Mart, 1966-

2004-01-01

Rets.rmt.: Oja, Martin., keelatud raamat : tekste 1996-2000. [Tallinn] : 9 Koma, [2003] ; Ilus, Peeter. Mõned luuletused. [Tallinn : Eesti Keele Sihtasutus, 2003] ; Klaus, Eduard. Pommikutsikas : [luuletused]. Tartu : Ilmamaa, 2003 ; Mathura, pseud. Sõstramesi : luuletusi. Külaküla [p.o. Tallinn] : Erakkond, 2003 ; Runnel, Simo. Uneriik : luuletused. Tartu : Ilmamaa, 2003

A description of the equipment for time-of-flight spectrum measurements on the fast reactor ZEBRA

International Nuclear Information System (INIS)

Gibson, I.H.; Jakeman, D.; Sanders, J.E.

1969-05-01

The pulsed source for the time-of-flight equipment consists of 14 MeV S-band linear electron accelerator, drift tube and water-cooled uranium-molybdenum alloy target installed on the ZEBRA lattice. Neutrons are extracted via a probe tube inserted into the core and an evacuated flight tube with counting stations at 50 m, 97 m and 200 m from the core centre. Two types of neutron detector are described and also the Perranti Argus 500 on-line computer which is used for data collection. The equipment is used for measuring the neutron energy spectra from the lowest energies up to about 1 MeV. (author)

The flights before the flight - An overview of shuttle astronaut training

Science.gov (United States)

Sims, John T.; Sterling, Michael R.

1989-01-01

Space shuttle astronaut training is centered at NASA's Johnson Space Center in Houston, Texas. Each astronaut receives many different types of training from many sources. This training includes simulator training in the Shuttle Mission Simulator, in-flight simulator training in the Shuttle Training Aircraft, Extravehicular Activity training in the Weightless Environment Training Facility and a variety of lectures and briefings. Once the training program is completed each shuttle flight crew is well-prepared to perform the normal operations required for their flight and deal with any shuttle system malfunctions that might occur.

The IRK time-of-flight facility for measurements of double-differential neutron emission cross sections

International Nuclear Information System (INIS)

Pavlik, A.; Priller, A.; Steier, P.; Vonach, H.; Winkler, G.

1994-01-01

In order to improve the present experimental data base of energy- and angle-differential neutron emission cross sections at 14 MeV incident-neutron energy, a new time-of-flight (TOF) facility was installed at the Institut fuer Radiumforschung und Kernphysik (IRK), Vienna. The set-up was particularly designed to more precisely measure the high-energy part of the secondary neutron spectra and consists of three main components: (1) a pulsed neutron generator of Cockcroft-Walton type producing primary neutrons via the T(d,n)-reaction, (2) a tube system which can be evacuated containing the neutron flight path, the sample, collimators and the sample positioning system, and (3) the neutron detectors with the data acquisition equipment. Removing the air along the neutron flight path results in a drastic suppression of background due to air-scattered neutrons in the spectrum of the secondary neutrons. For every secondary neutron detected in the main detector, the time-of-flight, the pulse-shape information and the recoil energy are recorded in list-mode via a CAMAC system connected to a PDP 11/34 on-line computer. Using a Micro VAX, the multiparameter data are sorted and reduced to double-differential cross sections

Implementation and flight tests for the Digital Integrated Automatic Landing System (DIALS). Part 1: Flight software equations, flight test description and selected flight test data

Science.gov (United States)

Hueschen, R. M.

1986-01-01

Five flight tests of the Digital Automated Landing System (DIALS) were conducted on the Advanced Transport Operating Systems (ATOPS) Transportation Research Vehicle (TSRV) -- a modified Boeing 737 aircraft for advanced controls and displays research. These flight tests were conducted at NASA's Wallops Flight Center using the microwave landing system (MLS) installation on runway 22. This report describes the flight software equations of the DIALS which was designed using modern control theory direct-digital design methods and employed a constant gain Kalman filter. Selected flight test performance data is presented for localizer (runway centerline) capture and track at various intercept angles, for glideslope capture and track of 3, 4.5, and 5 degree glideslopes, for the decrab maneuver, and for the flare maneuver. Data is also presented to illustrate the system performance in the presence of cross, gust, and shear winds. The mean and standard deviation of the peak position errors for localizer capture were, respectively, 24 feet and 26 feet. For mild wind conditions, glideslope and localizer tracking position errors did not exceed, respectively, 5 and 20 feet. For gusty wind conditions (8 to 10 knots), these errors were, respectively, 10 and 30 feet. Ten hands off automatic lands were performed. The standard deviation of the touchdown position and velocity errors from the mean values were, respectively, 244 feet and 0.7 feet/sec.

Theseus Landing Following Maiden Flight

Science.gov (United States)

1996-01-01

The Theseus prototype research aircraft shows off its high aspect-ratio wing as it comes in for a landing on Rogers Dry Lake after its first test flight from NASA's Dryden Flight Research Center, Edwards, California, on May 24, 1996. The Theseus aircraft, built and operated by Aurora Flight Sciences Corporation, Manassas, Virginia, was a unique aircraft flown at NASA's Dryden Flight Research Center, Edwards, California, under a cooperative agreement between NASA and Aurora. Dryden hosted the Theseus program, providing hangar space and range safety for flight testing. Aurora Flight Sciences was responsible for the actual flight testing, vehicle flight safety, and operation of the aircraft. The Theseus remotely piloted aircraft flew its maiden flight on May 24, 1996, at Dryden. During its sixth flight on November 12, 1996, Theseus experienced an in-flight structural failure that resulted in the loss of the aircraft. As of the beginning of the year 2000, Aurora had not rebuilt the aircraft. Theseus was built for NASA under an innovative, $4.9 million fixed-price contract by Aurora Flight Sciences Corporation and its partners, West Virginia University, Morgantown, West Virginia, and Fairmont State College, Fairmont, West Virginia. The twin-engine, unpiloted vehicle had a 140-foot wingspan, and was constructed largely of composite materials. Powered by two 80-horsepower, turbocharged piston engines that drove twin 9-foot-diameter propellers, Theseus was designed to fly autonomously at high altitudes, with takeoff and landing under the active control of a ground-based pilot in a ground control station 'cockpit.' With the potential ability to carry 700 pounds of science instruments to altitudes above 60,000 feet for durations of greater than 24 hours, Theseus was intended to support research in areas such as stratospheric ozone depletion and the atmospheric effects of future high-speed civil transport aircraft engines. Instruments carried aboard Theseus also would be able

Seltskond : [fotod] / tekst ja fotod Annika Haas

Index Scriptorium Estoniae

2008-01-01

29. mail tutvustasid autorid oma lasteraamatuid Eesti Lastekirjanduse Keskuses: Kass, Kristiina. Petra lood. [Tallinn] : Tänapäev, 2008 ; Vainola, Kätlin. Mia, Konrad ja avanevad uksed : [jutustus] / pildid joonistanud Toomas Pääsuke. [Tallinn] : Tänapäev, 2008 ; Saarna, Meelike. Mattias ja mamma. [Tallinn] : Tänapäev, 2008

212ʻ Fahrenheiti : eesti luule 2006 / Piret Bristol

Index Scriptorium Estoniae

Bristol, Piret, 1968-

2008-01-01

Järgmistest 2006. a. ilmunud luulekogudest: Ryytle, Indrek. Inglid rokijaamas. Puhja : I. Rüütle ; Runnel, Hando. Viru veri ei värise. Tartu : Ilmamaa ; Vabat, Martin. Mina olengi kirjandusklassik. Tartu : Eesti Kirjanduse Selts ; Korts, Eliina. Lööklaused murravad metsi. Tartu : Eesti Kirjanduse Selts ; Koff, Indrek. Vana laul. Luige : Verb ; Teede, Andra. Takso Tallinna taevas. Luige : Verb ; Vusser, Kaspar. Vusserduste võnked. Tallinn : P. Kukk ; Elbing, Andrus. Siin Beebilõust, tere! : häired pimelinna tänavalt = Ciao, it's Babyface : trouble from the streets of a blind city. Tallinn : Epifanio ; Hint, Miina. Vabaduse vang, ehk, Põrandaalune kirjandus. Tallinn : MR ; Jüriado, Tiiu. Luule on ime. Habaja : Kentaur ; Ligi, Katre. Naabrivalve. Tartu : Ilmamaa ; Krull, Hasso. Talv. Tallinn : Tuum ; Mets, Mae. Pühapäeval on reede. Tartu : Ilmamaa ; Ploom, Ülar. Porr ja sorry. Tallinn : Tuum ; Hirv, Indrek, Surmapõletaja. Tallinn : Tuum ; Piir, Milvi Martina. Kõrkjavaas. Tartu : Fantaasia ; Soomets, Triin. Väljas. Tallinn : Tuum ; Mathura. Kohalolu. Rapla : Allikäärne ; Afanasjev, Vahur. Katedraal Emajões. Tartu ; Brüssel : ID Salong//Sild, Ivar. Spermaga ja puha. Pärnu : Jumalikud Ilmutused ; Meiel, Kaupo. Polügrafisti käsiraamat. Pärnu : Jumalikud Ilmutused ; Kivisildnik, Sven. Vägistatud jäämägi. Pärnu : Jumalikud Ilmutused ; Arder, Ott. Luule sünnib kus sünnib kui sünnib / koost. Leelo Tungal. Tallinn : Tänapäev ; Kompus, Marko. Vallaliste jõgede tõkkejooksja. Tartu : M. Kompus

Cooperative random Levy flight searches and the flight patterns of honeybees

International Nuclear Information System (INIS)

Reynolds, A.M.

2006-01-01

The most efficient Levy flight (scale-free) searching strategy for N independent searchers to adopt when target sites are randomly and sparsely distributed is identified. For N=1, it is well known that the optimal searching strategy is attained when μ=2, where the exponent μ characterizes the Levy distribution, P(l)=l -μ , of flight-lengths. For N>1, the optimal searching strategy is attained as μ->1. It is suggested that the orientation flights of honeybees can be understood within the context of such an optimal cooperative random Levy flight searching strategy. Upon returning to their hive after surveying a landscape honeybees can exchange information about the locations of target sites through the waggle dance. In accordance with observations it is predicted that the waggle dance can be disrupted without noticeable influence on a hive's ability to maintain weight when forage is plentiful

[Micron]ADS-B Detect and Avoid Flight Tests on Phantom 4 Unmanned Aircraft System

Science.gov (United States)

Arteaga, Ricardo; Dandachy, Mike; Truong, Hong; Aruljothi, Arun; Vedantam, Mihir; Epperson, Kraettli; McCartney, Reed

2018-01-01

Researchers at the National Aeronautics and Space Administration Armstrong Flight Research Center in Edwards, California and Vigilant Aerospace Systems collaborated for the flight-test demonstration of an Automatic Dependent Surveillance-Broadcast based collision avoidance technology on a small unmanned aircraft system equipped with the uAvionix Automatic Dependent Surveillance-Broadcast transponder. The purpose of the testing was to demonstrate that National Aeronautics and Space Administration / Vigilant software and algorithms, commercialized as the FlightHorizon UAS"TM", are compatible with uAvionix hardware systems and the DJI Phantom 4 small unmanned aircraft system. The testing and demonstrations were necessary for both parties to further develop and certify the technology in three key areas: flights beyond visual line of sight, collision avoidance, and autonomous operations. The National Aeronautics and Space Administration and Vigilant Aerospace Systems have developed and successfully flight-tested an Automatic Dependent Surveillance-Broadcast Detect and Avoid system on the Phantom 4 small unmanned aircraft system. The Automatic Dependent Surveillance-Broadcast Detect and Avoid system architecture is especially suited for small unmanned aircraft systems because it integrates: 1) miniaturized Automatic Dependent Surveillance-Broadcast hardware; 2) radio data-link communications; 3) software algorithms for real-time Automatic Dependent Surveillance-Broadcast data integration, conflict detection, and alerting; and 4) a synthetic vision display using a fully-integrated National Aeronautics and Space Administration geobrowser for three dimensional graphical representations for ownship and air traffic situational awareness. The flight-test objectives were to evaluate the performance of Automatic Dependent Surveillance-Broadcast Detect and Avoid collision avoidance technology as installed on two small unmanned aircraft systems. In December 2016, four flight tests

Hüdra aastasada / Ene-Reet Soovik

Index Scriptorium Estoniae

Soovik, Ene-Reet

1997-01-01

Arvustus: Galsworthy, John. Peatüki lõpp : Üle jõe / tlk. Jüri ja Liisi Ojamaa. Tallinn : Eesti Raamat, 1997; Amis, Kingsley. qnneseen Jim / tlk. Urve Hanko. Tallinn : Eesti Raadio, 1997; Boyd, William. Sinine pärastlõuna / tlk. Virve Krimm. Tallinn : Varrak, 1997. Briti XX saj. kirjanduse ülevaade

POINT CLOUD ANALYSIS FOR UAV-BORNE LASER SCANNING WITH HORIZONTALLY AND VERTICALLY ORIENTED LINE SCANNERS – CONCEPT AND FIRST RESULTS

Directory of Open Access Journals (Sweden)

M. Weinmann

2017-08-01

Full Text Available In this paper, we focus on UAV-borne laser scanning with the objective of densely sampling object surfaces in the local surrounding of the UAV. In this regard, using a line scanner which scans along the vertical direction and perpendicular to the flight direction results in a point cloud with low point density if the UAV moves fast. Using a line scanner which scans along the horizontal direction only delivers data corresponding to the altitude of the UAV and thus a low scene coverage. For these reasons, we present a concept and a system for UAV-borne laser scanning using multiple line scanners. Our system consists of a quadcopter equipped with horizontally and vertically oriented line scanners. We demonstrate the capabilities of our system by presenting first results obtained for a flight within an outdoor scene. Thereby, we use a downsampling of the original point cloud and different neighborhood types to extract fundamental geometric features which in turn can be used for scene interpretation with respect to linear, planar or volumetric structures.

In-flight sleep, pilot fatigue and Psychomotor Vigilance Task performance on ultra-long range versus long range flights.

Science.gov (United States)

Gander, Philippa H; Signal, T Leigh; van den Berg, Margo J; Mulrine, Hannah M; Jay, Sarah M; Jim Mangie, Captain

2013-12-01

This study evaluated whether pilot fatigue was greater on ultra-long range (ULR) trips (flights >16 h on 10% of trips in a 90-day period) than on long range (LR) trips. The within-subjects design controlled for crew complement, pattern of in-flight breaks, flight direction and departure time. Thirty male Captains (mean age = 54.5 years) and 40 male First officers (mean age = 48.0 years) were monitored on commercial passenger flights (Boeing 777 aircraft). Sleep was monitored (actigraphy, duty/sleep diaries) from 3 days before the first study trip to 3 days after the second study trip. Karolinska Sleepiness Scale, Samn-Perelli fatigue ratings and a 5-min Psychomotor Vigilance Task were completed before, during and after every flight. Total sleep in the 24 h before outbound flights and before inbound flights after 2-day layovers was comparable for ULR and LR flights. All pilots slept on all flights. For each additional hour of flight time, they obtained an estimated additional 12.3 min of sleep. Estimated mean total sleep was longer on ULR flights (3 h 53 min) than LR flights (3 h 15 min; P(F) = 0.0004). Sleepiness ratings were lower and mean reaction speed was faster at the end of ULR flights. Findings suggest that additional in-flight sleep mitigated fatigue effectively on longer flights. Further research is needed to clarify the contributions to fatigue of in-flight sleep versus time awake at top of descent. The study design was limited to eastward outbound flights with two Captains and two First Officers. Caution must be exercised when extrapolating to different operations. © 2013 European Sleep Research Society.

VIEW FROM THE TOP: ENJOYABLE AND EFFECTIVE APPROACHES TO ELT FOR FLIGHT ATTENDANT

Directory of Open Access Journals (Sweden)

Nanik Rianandita Sari,S.S.,M.A.

2017-04-01

Full Text Available Young people today are more exposed to popular culture than any other age group. Television, movies, music, magazines, fashion, and internet form a major psychological part of the lives and life styles of youngsters. Since there has been increasing interest in the use of popular culture as aids in learning English. This research will investigate the ways in which popular culture might be used in teaching English. Learning language through pop culture, which comes from the West. Music, songs, and movies are highly popular with youngster. The movie ‘View From The Top‘, in particular, was a popular movie, where it entered the fantasy world of most young girl who want to be a flight attendant class of 2011. Many of flight attendant watch this movie for several times, remembering the lines spoken by the actress, and reciting the lyrics of the theme songs. All of which seems to suggest that flight attendant student can learn English through their encounters with popular culture. A movie is one interesting way to learn English. Movie is one of popular culture which is part of oral literature which enhances ELT through elements such as authentic material, language in use and aesthetic representation of the spoken language, as well as language and cultural enrichment. Literature appeals to flight attendant students, it motivates them to become responsive and active learners.

The Orion Exploration Flight Test Post Flight Solid Particle Flight Environment Inspection and Analysis

Science.gov (United States)

Miller, Joshua E.

2016-01-01

Orbital debris in the millimeter size range can pose a hazard to current and planned spacecraft due to the high relative impact speeds in Earth orbit. Fortunately, orbital debris has a relatively short life at lower altitudes due to atmospheric effects; however, at higher altitudes orbital debris can survive much longer and has resulted in a band of high flux around 700 to 1,500 km above the surface of the Earth. While large orbital debris objects are tracked via ground based observation, little information can be gathered about small particles except by returned surfaces, which until the Orion Exploration Flight Test number one (EFT-1), has only been possible for lower altitudes (400 to 500 km). The EFT-1 crew module backshell, which used a porous, ceramic tile system with surface coatings, has been inspected post-flight for potential micrometeoroid and orbital debris (MMOD) damage. This paper describes the pre- and post-flight activities of inspection, identification and analysis of six candidate MMOD impact craters from the EFT-1 mission.

Manned Flight Simulator (MFS)

Data.gov (United States)

Federal Laboratory Consortium — The Aircraft Simulation Division, home to the Manned Flight Simulator (MFS), provides real-time, high fidelity, hardware-in-the-loop flight simulation capabilities...

NASA/FAA/NCAR Supercooled Large Droplet Icing Flight Research: Summary of Winter 1996-1997 Flight Operations

Science.gov (United States)

Miller, Dean; Ratvasky, Thomas; Bernstein, Ben; McDonough, Frank; Strapp, J. Walter

1998-01-01

During the winter of 1996-1997, a flight research program was conducted at the NASA-Lewis Research Center to study the characteristics of Supercooled Large Droplets (SLD) within the Great Lakes region. This flight program was a joint effort between the National Aeronautics and Space Administration (NASA), the National Center for Atmospheric Research (NCAR), and the Federal Aviation Administration (FAA). Based on weather forecasts and real-time in-flight guidance provided by NCAR, the NASA-Lewis Icing Research Aircraft was flown to locations where conditions were believed to be conducive to the formation of Supercooled Large Droplets aloft. Onboard instrumentation was then used to record meteorological, ice accretion, and aero-performance characteristics encountered during the flight. A total of 29 icing research flights were conducted, during which "conventional" small droplet icing, SLD, and mixed phase conditions were encountered aloft. This paper will describe how flight operations were conducted, provide an operational summary of the flights, present selected experimental results from one typical research flight, and conclude with practical "lessons learned" from this first year of operation.

In-flight Assessment of Lower Body Negative Pressure as a Countermeasure for Post-flight Orthostatic Intolerance

Science.gov (United States)

Charles, J. B.; Stenger, M. B.; Phillips, T. R.; Arzeno, N. M.; Lee, S. M. C.

2009-01-01

Introduction. We investigated the efficacy of combining fluid loading with sustained lower body negative pressure (LBNP) to reverse orthostatic intolerance associated with weightlessness during and immediately after Space Shuttle missions. Methods. Shuttle astronauts (n=13) underwent 4 hours of LBNP at -30 mm(Hg) and ingested water and salt ( soak treatment) during flight in two complementary studies. In the first study (n=8), pre-flight heart rate (HR) and blood pressure (BP) responses to an LBNP ramp (5-min stages of -10 mm(Hg) steps to -50 mm(Hg) were compared to responses in-flight one and two days after LBNP soak treatment. In the second study (n=5), the soak was performed 24 hr before landing, and post-flight stand test results of soak subjects were compared with those of an untreated cohort (n=7). In both studies, the soak was scheduled late in the mission and was preceded by LBNP ramp tests at approximately 3-day intervals to document the in-flight loss of orthostatic tolerance. Results. Increased HR and decreased BP responses to LBNP were evident early in-flight. In-flight, one day after LBNP soak, HR and BP responses to LBNP were not different from pre-flight, but the effect was absent the second day after treatment. Post-flight there were no between-group differences in HR and BP responses to standing, but all 5 treatment subjects completed the 5-minute stand test whereas 2 of 7 untreated cohort subjects did not. Discussion. Exaggerated HR and BP responses to LBNP were evident within the first few days of space flight, extending results from Skylab. The combined LBNP and fluid ingestion countermeasure restored in-flight LBNP HR and BP responses to pre-flight levels and provided protection of post-landing orthostatic function. Unfortunately, any benefits of the combined countermeasure were offset by the complexity of its implementation, making it inappropriate for routine application during Shuttle flights.

Kolmanda raamatu kiituseks / Peeter Olesk

Index Scriptorium Estoniae

Olesk, Peeter, 1953-

2009-01-01

Tutvustus: Isaacson, Walter. Einstein : tema elu ja universum / tõlkinud Matti Piirimaa. Tallinn : Eesti Raamat, 2009; Fortey, Jacqueline. Kuulsad teadlased (Silmaring) / tõlkinud Ülle Haav ja Helen Haav. Tallinn : Koolibri, 2009; Vaim ja aeg (Lehed ja tähed : looduse ja teaduse aastaraamat, 5) / koostanud Indrek Rohtmets ja Toomas Kukk. Tallinn : Loodusajakiri, 2009

Tõde jälitab meid kui vari / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

2006-01-01

Erich Maria Remarque'ist seoses romaani "Lissaboni öö" kordustrüki ilmumisega (kirj. Tänapäev). Raamatututvustused: Vaarandi, Debora. Aastad ja päevad : nooruselugu. Tallinn : Tänapäev, 2006 ; Loosaar, Evald. Eesti mehe lugu. Tallinn : Varrak, 2006 ; Kangro, Bernard, Ristikivi, Karl. Kirjad romaanist : 31 kirja aastaist 1966-1977. Tallinn : Varrak, 2006

Short Outlines of Books by Estonian Authors / Janika Kronberg, Rutt Hinrikus

Index Scriptorium Estoniae

Kronberg, Janika, 1963-

2009-01-01

Arvustus: Kaplinski, Jaan. Parallelle ja parallelisme. Tartu : Tartu Ülikooli Kirjastus, c2009 ; Hellat, Henn-Kaarel. Inimese tegemine I-V. Tallinn : Faatum, 2002-2008 ; Nõu, Helga. Elu täis üllatusi. Tartu : Atlex, 2009 ; Remsu, Olev. Musketäride muundumised. [Tallinn] : Eesti Keele Sihtasutus, 2008 ; Ristikivi, Karl. Päevaraamat 1957-1968. Tallinn : Varrak, 2008

Küülikud jooksus ja jumal surnud : eesti lasteproosa tipud on "kuldaja" autoritega võrdväärsed / Jürgen Rooste

Index Scriptorium Estoniae

Rooste, Jürgen, 1979-

2005-01-01

Arvustus: Raud, Piret. Ernesto küülikud. Tallinn : Tänapäev, 2004 ; Soans, Kerttu. Kruubi-Ruudi ja tema inimesed. Puhja : Väike Vanker, 2004 ; Kivirähk, Andrus. Limpa ja mereröövlid. Tallinn : Varrak, 2004 ; Sauter, Peeter. Laste raamat / Rull ja Ekke ja Pipa ja Peeter Sauter. Tallinn : Huma, 2004

Raamat / Matis Rodin

Index Scriptorium Estoniae

Rodin, Matis

2012-01-01

Raamatututvustus: Paulus, Karin. Tootedisain : asjad minu elus. Tallinn : Eesti Kunstiakadeemia, 2011; Vainküla, Tõnu, Pere, René. Vana mööbel korda oma kätega. [Tallinn] : Ajakirjade Kirjastus, 2012; Ruumipilt 2011 : Eesti parimad interjöörid ja disain / Eesti Sisearhitektide Liit ; toimetaja ja vastutav väljaandja Priit Põldme. Tallinn, 2012

Vision based flight procedure stereo display system

Science.gov (United States)

Shen, Xiaoyun; Wan, Di; Ma, Lan; He, Yuncheng

2008-03-01

A virtual reality flight procedure vision system is introduced in this paper. The digital flight map database is established based on the Geographic Information System (GIS) and high definitions satellite remote sensing photos. The flight approaching area database is established through computer 3D modeling system and GIS. The area texture is generated from the remote sensing photos and aerial photographs in various level of detail. According to the flight approaching procedure, the flight navigation information is linked to the database. The flight approaching area vision can be dynamic displayed according to the designed flight procedure. The flight approaching area images are rendered in 2 channels, one for left eye images and the others for right eye images. Through the polarized stereoscopic projection system, the pilots and aircrew can get the vivid 3D vision of the flight destination approaching area. Take the use of this system in pilots preflight preparation procedure, the aircrew can get more vivid information along the flight destination approaching area. This system can improve the aviator's self-confidence before he carries out the flight mission, accordingly, the flight safety is improved. This system is also useful in validate the visual flight procedure design, and it helps to the flight procedure design.

Review on flight simulators (today and tomorrow); Flight simulatior no genjo to kongo

Energy Technology Data Exchange (ETDEWEB)

Komura, T. [Mitsubishi Precision Company Limited, Tokyo (Japan)

2000-04-05

This paper presents various flight simulators. A flight simulator is classified into that for R and D on aircraft and that for flight training according to its usage. As an example of the former, the general-purpose flight simulation test facility of National Aerospace Laboratory, Science and Technology Agency is in use for development of the STOL experimental aircraft 'Asuka' and simulation experiments for space development. A civil aircraft simulator simulating the interior of a cockpit, operation feeling of piloting devices, flight performance, dynamic characteristics, an engine system and a hydraulic system like a real aircraft is in wide use for training pilots. A fighter simulator for air force is used for training detection of enemy's aircraft by radar, and missile shooting. An antisubmarine patrol aircraft simulator is used for training detection of submarines by sonic detector and magnetic detector, and torpedo air-launching. For both simulators, real simulation of detection sensors or battle environment is required. (NEDO)

Flight Muscle Dimorphism and Heterogeneity in Flight Initiation of Field-Collected Triatoma infestans (Hemiptera: Reduviidae)

OpenAIRE

Gurevitz, Juan M.; Kitron, Uriel; Gürtler, Ricardo E.

2007-01-01

Recent experiments demonstrated that most field-collected Triatoma infestans (Klug) (Hemiptera: Reduviidae) adults from northern Argentina either never initiated flight or did so repeatedly in both sexes. This pattern could not be explained by sex, adult age, weight, weight-to-length ratio (W/L), or chance. We examined whether bugs that never initiated flight possessed developed flight muscles, and whether flight muscle mass relative to total body mass (FMR) was related to the probability of ...

14 CFR 27.151 - Flight controls.

Science.gov (United States)

2010-01-01

... 14 Aeronautics and Space 1 2010-01-01 2010-01-01 false Flight controls. 27.151 Section 27.151... STANDARDS: NORMAL CATEGORY ROTORCRAFT Flight Flight Characteristics § 27.151 Flight controls. (a) Longitudinal, lateral, directional, and collective controls may not exhibit excessive breakout force, friction...

14 CFR 29.151 - Flight controls.

Science.gov (United States)

2010-01-01

... 14 Aeronautics and Space 1 2010-01-01 2010-01-01 false Flight controls. 29.151 Section 29.151... STANDARDS: TRANSPORT CATEGORY ROTORCRAFT Flight Flight Characteristics § 29.151 Flight controls. (a) Longitudinal, lateral, directional, and collective controls may not exhibit excessive breakout force, friction...

Capital Flight from Russia

OpenAIRE

Prakash Loungani; Paolo Mauro

2000-01-01

This paper documents the scale of capital flight from Russia, compares it with that observed in other countries, and reviews policy options. The evidence from other countries suggests that capital flight can be reversed once reforms take hold. The paper argues that capital flight from Russia can only be curbed through a medium-term reform strategy aimed at improving governance and macroeconomic performance, and strengthening the banking system. Capital controls result in costly distortions an...

Passengers waste production during flights.

Science.gov (United States)

Tofalli, Niki; Loizia, Pantelitsa; Zorpas, Antonis A

2017-12-20

We assume that during flights the amount of waste that is produced is limited. However, daily, approximately 8000 commercial airplanes fly above Europe's airspace while at the same time, more than 17,000 commercial flights exist in the entire world. Using primary data from airlines, which use the Larnaca's International Airport (LIA) in Cyprus, we have tried to understand why wastes are produced during a typical flight such as food waste, paper, and plastics, as well as how passengers affect the production of those wastes. The compositional analysis took place on 27 flights of 4 different airlines which used LIA as final destination. The evaluation indicated that the passenger's habits and ethics, and the policy of each airline produced different kinds of waste during the flights and especially food waste (FW). Furthermore, it was observed that the only waste management strategy that exists in place in the airport is the collection and the transportation of all those wastes from aircrafts and from the airport in the central unit for further treatment. Hence, this research indicated extremely difficulties to implement any specific waste minimization, or prevention practice or other sorting methods during the flights due to the limited time of the most flights (less than 3 h), the limited available space within the aircrafts, and the strictly safety roles that exist during the flights.

A Flight Control System Architecture for the NASA AirSTAR Flight Test Infrastructure

Science.gov (United States)

Murch, Austin M.

2008-01-01

A flight control system architecture for the NASA AirSTAR infrastructure has been designed to address the challenges associated with safe and efficient flight testing of research control laws in adverse flight conditions. The AirSTAR flight control system provides a flexible framework that enables NASA Aviation Safety Program research objectives, and includes the ability to rapidly integrate and test research control laws, emulate component or sensor failures, inject automated control surface perturbations, and provide a baseline control law for comparison to research control laws and to increase operational efficiency. The current baseline control law uses an angle of attack command augmentation system for the pitch axis and simple stability augmentation for the roll and yaw axes.

Operational Lessons Learned from the Ares I-X Flight Test

Science.gov (United States)

Davis, Stephan R.

2010-01-01

The Ares I-X flight test, launched in 2009, is the first test of the Ares I crew launch vehicle. This development flight test evaluated the flight dynamics, roll control, and separation events, but also provided early insights into logistical, stacking, launch, and recovery operations for Ares I. Operational lessons will be especially important for NASA as the agency makes the transition from the Space Shuttle to the Constellation Program, which is designed to be less labor-intensive. The mission team itself comprised only 700 individuals over the life of the project compared to the thousands involved in Shuttle and Apollo missions; while missions to and beyond low-Earth orbit obviously will require additional personnel, this lean approach will serve as a model for future Constellation missions. To prepare for Ares I-X, vehicle stacking and launch infrastructure had to be modified at Kennedy Space Center's Vehicle Assembly Building (VAB) as well as Launch Complex (LC) 39B. In the VAB, several platforms and other structures designed for the Shuttle s configuration had to be removed to accommodate the in-line, much taller Ares I-X. Vehicle preparation activities resulted in delays, but also in lessons learned for ground operations personnel, including hardware deliveries, cable routing, transferred work and custodial paperwork. Ares I-X also proved to be a resource challenge, as individuals and ground service equipment (GSE) supporting the mission also were required for Shuttle or Atlas V operations at LC 40/41 at Cape Canaveral Air Force Station. At LC 39B, several Shuttle-specific access arms were removed and others were added to accommodate the in-line Ares vehicle. Ground command, control, and communication (GC3) hardware was incorporated into the Mobile Launcher Platform (MLP). The lightning protection system at LC 39B was replaced by a trio of 600-foot-tall towers connected by a catenary wire to account for the much greater height of the vehicle. Like Shuttle

Free Flight Rotorcraft Flight Test Vehicle Technology Development

Science.gov (United States)

Hodges, W. Todd; Walker, Gregory W.

1994-01-01

A rotary wing, unmanned air vehicle (UAV) is being developed as a research tool at the NASA Langley Research Center by the U.S. Army and NASA. This development program is intended to provide the rotorcraft research community an intermediate step between rotorcraft wind tunnel testing and full scale manned flight testing. The technologies under development for this vehicle are: adaptive electronic flight control systems incorporating artificial intelligence (AI) techniques, small-light weight sophisticated sensors, advanced telepresence-telerobotics systems and rotary wing UAV operational procedures. This paper briefly describes the system's requirements and the techniques used to integrate the various technologies to meet these requirements. The paper also discusses the status of the development effort. In addition to the original aeromechanics research mission, the technology development effort has generated a great deal of interest in the UAV community for related spin-off applications, as briefly described at the end of the paper. In some cases the technologies under development in the free flight program are critical to the ability to perform some applications.

76 FR 16236 - Prohibition Against Certain Flights Within the Tripoli (HLLL) Flight Information Region (FIR)

Science.gov (United States)

2011-03-23

... Tripoli (HLLL) Flight Information Region (FIR) AGENCY: Federal Aviation Administration (FAA), Department... the Tripoli (HLLL) Flight Information Region (FIR) by all U.S. air carriers; U.S. commercial operators...) Flight Information Region (FIR). (a) Applicability. This section applies to the following persons: (1...

78 FR 66261 - Certified Flight Instructor Flight Reviews; Recent Pilot in Command Experience; Airmen Online...

Science.gov (United States)

2013-11-05

...-0780; Amdt. No. 61-131] RIN 2120-AK23 Certified Flight Instructor Flight Reviews; Recent Pilot in Command Experience; Airmen Online Services; Confirmation of Effective Date AGENCY: Federal Aviation...-calendar month flight review requirements. This rule also clarifies that the generally applicable recent...

78 FR 56822 - Certified Flight Instructor Flight Reviews; Recent Pilot in Command Experience; Airmen Online...

Science.gov (United States)

2013-09-16

...-0780; Amdt. No. 61-131] RIN 2120-AK23 Certified Flight Instructor Flight Reviews; Recent Pilot in Command Experience; Airmen Online Services AGENCY: Federal Aviation Administration (FAA), DOT. ACTION... review requirements. This rule also clarifies that the generally applicable recent flight experience...

Flight to Safety from European Stock Markets

DEFF Research Database (Denmark)

Aslanidis, Nektarios; Christiansen, Charlotte

-return trade-off is positive and during flight-to-safety episodes it is negative. The effects of flight-to-safety episodes on the risk-return trade-off are qualitatively similar for own country flight-to-safety episodes, for flight from own country stock market to the US bond market, and for US flight......This paper investigates flight-to-safety from stocks to bonds in seven European markets. We use quantile regressions to identify flight-to-safety episodes. The simple risk-return trade-off on the stock markets is negative which is caused by flight-to-safety episodes: During normal periods, the risk...

Asset Analysis and Operational Concepts for Separation Assurance Flight Testing at Dryden Flight Research Center

Science.gov (United States)

Costa, Guillermo J.; Arteaga, Ricardo A.

2011-01-01

A preliminary survey of existing separation assurance and collision avoidance advancements, technologies, and efforts has been conducted in order to develop a concept of operations for flight testing autonomous separation assurance at Dryden Flight Research Center. This effort was part of the Unmanned Aerial Systems in the National Airspace System project. The survey focused primarily on separation assurance projects validated through flight testing (including lessons learned), however current forays into the field were also examined. Comparisons between current Dryden flight and range assets were conducted using House of Quality matrices in order to allow project management to make determinations regarding asset utilization for future flight tests. This was conducted in order to establish a body of knowledge of the current collision avoidance landscape, and thus focus Dryden s efforts more effectively towards the providing of assets and test ranges for future flight testing within this research field.

Solar array flight dynamic experiment

Science.gov (United States)

Schock, Richard W.

1987-01-01

The purpose of the Solar Array Flight Dynamic Experiment (SAFDE) is to demonstrate the feasibility of on-orbit measurement and ground processing of large space structures' dynamic characteristics. Test definition or verification provides the dynamic characteristic accuracy required for control systems use. An illumination/measurement system was developed to fly on space shuttle flight STS-41D. The system was designed to dynamically evaluate a large solar array called the Solar Array Flight Experiment (SAFE) that had been scheduled for this flight. The SAFDE system consisted of a set of laser diode illuminators, retroreflective targets, an intelligent star tracker receiver and the associated equipment to power, condition, and record the results. In six tests on STS-41D, data was successfully acquired from 18 retroreflector targets and ground processed, post flight, to define the solar array's dynamic characteristic. The flight experiment proved the viability of on-orbit test definition of large space structures dynamic characteristics. Future large space structures controllability should be greatly enhanced by this capability.

Moodsa luule maailmakeel / Märt Väljataga

Index Scriptorium Estoniae

Väljataga, Märt, 1965-

2007-01-01

Magrelli, Valerio. Luule DNA = Il DNE della poesia / tõlkinudk Maarja Kangro ja Kalju Kruusa. Tallinn : Koma, 2006 ; Enzensberger, Hans. Tõmba sobimatu maha : [luuletused] / saksa keelest tõlkinud [ja järelsõna:] Maarja Kangro. Tallinn : Kultuurileht, 2006 ; Kronbergs, Juris. Maa-alune luule / läti keelest tõlkinud Guntars Godinsh, Livia Viitol. Tallinn : Kultuurileht, 2007

System Identification of Flight Mechanical Characteristics

OpenAIRE

Larsson, Roger

2013-01-01

With the demand for more advanced fighter aircraft, relying on relaxed stability or even unstable flight mechanical characteristics to gain flight performance, more focus has been put on model-based system engineering to help with the design work. The flight control system design is one important part that relies on this modeling. Therefore it has become more important to develop flight mechanical models that are highly accurate in the whole flight envelop. For today’s newly developed fighter...

Completely optical orientation determination for an unstabilized aerial three-line camera

Science.gov (United States)

Wohlfeil, Jürgen

2010-10-01

Aerial line cameras allow the fast acquisition of high-resolution images at low costs. Unfortunately the measurement of the camera's orientation with the necessary rate and precision is related with large effort, unless extensive camera stabilization is used. But also stabilization implicates high costs, weight, and power consumption. This contribution shows that it is possible to completely derive the absolute exterior orientation of an unstabilized line camera from its images and global position measurements. The presented approach is based on previous work on the determination of the relative orientation of subsequent lines using optical information from the remote sensing system. The relative orientation is used to pre-correct the line images, in which homologous points can reliably be determined using the SURF operator. Together with the position measurements these points are used to determine the absolute orientation from the relative orientations via bundle adjustment of a block of overlapping line images. The approach was tested at a flight with the DLR's RGB three-line camera MFC. To evaluate the precision of the resulting orientation the measurements of a high-end navigation system and ground control points are used.

Aerodynamics of bird flight

Directory of Open Access Journals (Sweden)

Dvořák Rudolf

2016-01-01

Full Text Available Unlike airplanes birds must have either flapping or oscillating wings (the hummingbird. Only such wings can produce both lift and thrust – two sine qua non attributes of flying.The bird wings have several possibilities how to obtain the same functions as airplane wings. All are realized by the system of flight feathers. Birds have also the capabilities of adjusting the shape of the wing according to what the immediate flight situation demands, as well as of responding almost immediately to conditions the flow environment dictates, such as wind gusts, object avoidance, target tracking, etc. In bird aerodynamics also the tail plays an important role. To fly, wings impart downward momentum to the surrounding air and obtain lift by reaction. How this is achieved under various flight situations (cruise flight, hovering, landing, etc., and what the role is of the wing-generated vortices in producing lift and thrust is discussed.The issue of studying bird flight experimentally from in vivo or in vitro experiments is also briefly discussed.

Production Support Flight Control Computers: Research Capability for F/A-18 Aircraft at Dryden Flight Research Center

Science.gov (United States)

Carter, John F.

1997-01-01

NASA Dryden Flight Research Center (DFRC) is working with the United States Navy to complete ground testing and initiate flight testing of a modified set of F/A-18 flight control computers. The Production Support Flight Control Computers (PSFCC) can give any fleet F/A-18 airplane an in-flight, pilot-selectable research control law capability. NASA DFRC can efficiently flight test the PSFCC for the following four reasons: (1) Six F/A-18 chase aircraft are available which could be used with the PSFCC; (2) An F/A-18 processor-in-the-loop simulation exists for validation testing; (3) The expertise has been developed in programming the research processor in the PSFCC; and (4) A well-defined process has been established for clearing flight control research projects for flight. This report presents a functional description of the PSFCC. Descriptions of the NASA DFRC facilities, PSFCC verification and validation process, and planned PSFCC projects are also provided.

Orion Exploration Flight Test Reaction Control System Jet Interaction Heating Environment from Flight Data

Science.gov (United States)

White, Molly E.; Hyatt, Andrew J.

2016-01-01

The Orion Multi-Purpose Crew Vehicle (MPCV) Reaction Control System (RCS) is critical to guide the vehicle along the desired trajectory during re-­-entry. However, this system has a significant impact on the convective heating environment to the spacecraft. Heating augmentation from the jet interaction (JI) drives thermal protection system (TPS) material selection and thickness requirements for the spacecraft. This paper describes the heating environment from the RCS on the afterbody of the Orion MPCV during Orion's first flight test, Exploration Flight Test 1 (EFT-1). These jet plumes interact with the wake of the crew capsule and cause an increase in the convective heating environment. Not only is there widespread influence from the jet banks, there may also be very localized effects. The firing history during EFT-1 will be summarized to assess which jet bank interaction was measured during flight. Heating augmentation factors derived from the reconstructed flight data will be presented. Furthermore, flight instrumentation across the afterbody provides the highest spatial resolution of the region of influence of the individual jet banks of any spacecraft yet flown. This distribution of heating augmentation across the afterbody will be derived from the flight data. Additionally, trends with possible correlating parameters will be investigated to assist future designs and ground testing programs. Finally, the challenges of measuring JI, applying this data to future flights and lessons learned will be discussed.

Kirjanik ja pasatornaado I / Tiit Aleksejev

Index Scriptorium Estoniae

Aleksejev, Tiit, 1968-

2008-01-01

Vene kodusõja kajastamisest 1920. aastate nõukogude proosas. Käsitletakse Isaak Babeli novellikogu "Ratsaarmee" (tõlkinud Olev Jõgi. Tallinn : Eesti Raamat, 1977), Boriss Lavrenjovi jutustust "Neljakümne esimene" (tõlkinud Jüri Karindi. Tallinn : Eesti Raamat, 1975), Viktor Kini jutustust "Valgete tagalas" (tõlkinud Jüri Ojamaa. Tallinn : Eesti Raamat, 1978), Hubert Minagrelli jutustust "Neli sõdurit" (pr. k. "Quatre soldats"), Andrei Platonovi novelli "Inimene iseendas" (ilmunud raamatus "Meistri saamine" / tõlkinud Virve Krimm. Tallinn : Eesti Raamat, 1979) ja romaani "Tševengur" (ilmunud raamatus "Tševengur. Kotlovan. Rasskazõ". Moskva, 2007), samuti ka Arkadi Gaidari loomingut

Flight testing a propulsion-controlled aircraft emergency flight control system on an F-15 airplane

Science.gov (United States)

Burcham, F. W., Jr.; Burken, John; Maine, Trindel A.

1994-01-01

Flight tests of a propulsion-controlled aircraft (PCA) system on an F-15 airplane have been conducted at the NASA Dryden Flight Research Center. The airplane was flown with all flight control surfaces locked both in the manual throttles-only mode and in an augmented system mode. In the latter mode, pilot thumbwheel commands and aircraft feedback parameters were used to position the throttles. Flight evaluation results showed that the PCA system can be used to land an airplane that has suffered a major flight control system failure safely. The PCA system was used to recover the F-15 airplane from a severe upset condition, descend, and land. Pilots from NASA, U.S. Air Force, U.S. Navy, and McDonnell Douglas Aerospace evaluated the PCA system and were favorably impressed with its capability. Manual throttles-only approaches were unsuccessful. This paper describes the PCA system operation and testing. It also presents flight test results and pilot comments.

Investigation of controlled flight into terrain : descriptions of flight paths for selected controlled flight into terrain (CFIT) aircraft accidents, 1985-1997

Science.gov (United States)

1999-03-01

This report documents an investigation of the flight paths of 13 selected controlled flight into terrain (CFIT) aircraft accidents that occurred between 1985 and 1997. The Operations Assessment Division (DTS-43) and the Aviation Safety Division (DTS-...

The development of a Flight Test Engineer's Workstation for the Automated Flight Test Management System

Science.gov (United States)

Tartt, David M.; Hewett, Marle D.; Duke, Eugene L.; Cooper, James A.; Brumbaugh, Randal W.

1989-01-01

The Automated Flight Test Management System (ATMS) is being developed as part of the NASA Aircraft Automation Program. This program focuses on the application of interdisciplinary state-of-the-art technology in artificial intelligence, control theory, and systems methodology to problems of operating and flight testing high-performance aircraft. The development of a Flight Test Engineer's Workstation (FTEWS) is presented, with a detailed description of the system, technical details, and future planned developments. The goal of the FTEWS is to provide flight test engineers and project officers with an automated computer environment for planning, scheduling, and performing flight test programs. The FTEWS system is an outgrowth of the development of ATMS and is an implementation of a component of ATMS on SUN workstations.

First on-line applications of a multi-reflection time-of-flight mass separator at ISOLTRAP and the mass measurement of 82Zn

International Nuclear Information System (INIS)

Wolf, Robert

2013-01-01

This thesis describes the implementation and first on-line application of a multi-reflection time-of-flight (MR-ToF) mass analyzer for high-resolution mass separation at the ISOLTRAP mass spectrometer at ISOLDE/CERN. On the one hand, the major objective was to improve ISOLTRAPs mass-measurement capabilities with respect to the ratio of delivered contaminating ions to ions of interest. On the other hand, the time necessary to purify wanted from unwanted species should be reduced as much as possible to enable access to even more exotic nuclei. The device has been set up, optimized and tested at the University of Greifswald before its move to ISOLTRAP. The achieved performance comprises mass resolving powers of up to 2 x 10 5 reached at observation times of 30 ms and a contamination suppression of about four orders of magnitude by use of a Bradbury-Nielsen gate. With the characteristics, it outperforms clearly the so far state-of-the-art purification method of a gas-filled Penning trap. To improve the utilization of the MR-ToF mass analyzer, the in-trap lift method has been developed. It simplifies the application and optimization of the device, which is a crucial time factor in an on-line experiment. The device was the first of its kind successfully applied to radioactive ion beams for a mass analysis, for a mass separation (in combination with the Bradbury-Nielsen gate) as a preparatory step for a subsequent Penning-trap mass measurement and as a high-precision mass spectrometer of its own. The later was recently used for the first mass measurement of the neutron-rich calcium isotopes 53 Ca and 54 Ca. The so-far achieved mass-resolving power of 2 x 10 5 belongs to the highest reported for time-of-flight mass analyzers at all. The first successful application of the MR-ToF system as the only mass separator at ISOLTRAP resulted in the mass measurement of 82 Zn. The new mass value has been compared to mass extrapolations of the most recent Hartree-Fock-Bogolyubov (HFB

14 CFR 141.41 - Flight simulators, flight training devices, and training aids.

Science.gov (United States)

2010-01-01

..., and training aids. 141.41 Section 141.41 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION... aids. An applicant for a pilot school certificate or a provisional pilot school certificate must show that its flight simulators, flight training devices, training aids, and equipment meet the following...

The use of an automated flight test management system in the development of a rapid-prototyping flight research facility

Science.gov (United States)

Duke, Eugene L.; Hewett, Marle D.; Brumbaugh, Randal W.; Tartt, David M.; Antoniewicz, Robert F.; Agarwal, Arvind K.

1988-01-01

An automated flight test management system (ATMS) and its use to develop a rapid-prototyping flight research facility for artificial intelligence (AI) based flight systems concepts are described. The ATMS provides a flight test engineer with a set of tools that assist in flight planning and simulation. This system will be capable of controlling an aircraft during the flight test by performing closed-loop guidance functions, range management, and maneuver-quality monitoring. The rapid-prototyping flight research facility is being developed at the Dryden Flight Research Facility of the NASA Ames Research Center (Ames-Dryden) to provide early flight assessment of emerging AI technology. The facility is being developed as one element of the aircraft automation program which focuses on the qualification and validation of embedded real-time AI-based systems.

14 CFR 63.43 - Flight engineer courses.

Science.gov (United States)

2010-01-01

... 14 Aeronautics and Space 2 2010-01-01 2010-01-01 false Flight engineer courses. 63.43 Section 63...) AIRMEN CERTIFICATION: FLIGHT CREWMEMBERS OTHER THAN PILOTS Flight Engineers § 63.43 Flight engineer courses. An applicant for approval of a flight engineer course must submit a letter to the Administrator...

Design and utilization of a Flight Test Engineering Database Management System at the NASA Dryden Flight Research Facility

Science.gov (United States)

Knighton, Donna L.

1992-01-01

A Flight Test Engineering Database Management System (FTE DBMS) was designed and implemented at the NASA Dryden Flight Research Facility. The X-29 Forward Swept Wing Advanced Technology Demonstrator flight research program was chosen for the initial system development and implementation. The FTE DBMS greatly assisted in planning and 'mass production' card preparation for an accelerated X-29 research program. Improved Test Plan tracking and maneuver management for a high flight-rate program were proven, and flight rates of up to three flights per day, two times per week were maintained.

Malle Talveti huvitavad naised / Kärt Hellerma

Index Scriptorium Estoniae

Hellerma, Kärt, 1956-

2006-01-01

Arvustus: McCullers, Carson. Laulatuse lummas / tõlk. Malle Talvet. Tallinn : Perioodika, 1988. (Loomingu Raamatukogu ; 1988, 3-5) ; Duras, Marguerite. Armuke / tõlk. Malle Talvet. Tallinn : Perioodika, 1988. (Loomingu Raamatukogu ; 1988, 11-12) ; Brookner, Anita. Hotel du Lac / tõlk. Malle Talvet. Tallinn : Perioodika, 1990. (Loomingu Raamatukogu ; 1990, 45-46). Varem ilmunud: Eesti Elu nr. 1 (13), 1. veebruar 1991

Kirjanik soovitab / Heiki Vilep

Index Scriptorium Estoniae

Vilep, Heiki, 1960-

2009-01-01

Tutvustus: Pratt, David. Võimatu nõuab rohkem aega : 1000 tarkusetera Nobeli preemia laureaadilt / inglise keelest tõlkinud Marge Paal. [Tallinn] : Ersen, 2009 ; Varblane, Hannes. Taarnateel : katsetusi 1967–1970 : [luuletused]. Tartu : Ilmamaa, 2009 ; Eesti muinasjuttude kuldraamat / koostanud Reet Krusten. Tallinn : TEA Kirjastus, 2009 ; Eco, Umberto. Kuus jalutuskäiku kirjandusmetsades / inglise keelest tõlkinud Ene-Reet Soovik. Tallinn : Varrak, 2009

[Raamatute tutvustus] / Tiit Pruuli

Index Scriptorium Estoniae

Pruuli, Tiit, 1965-

2010-01-01

Tutvustus: Asmus, Ronald D. Väike sõda, mis raputas maailma. Gruusia, Venemaa ja Lääne tulevik. Tallinn : Eesti Ajalehed, 2010 ; Ševardnadze, Eduard. Kui raudne eesriie rebenes. Tallinn : Olion, 2009 ; Vene-Gruusia sõda 08.08.2008. Kuidas see tegelikkuses oli. Tallinn : Kniga.ee, 2010 ; Raudam, Dagmar. Minu Gruusia. Elu nagu mägitee. Tartu : Petrone Print, 2010

Väike luulekaleidoskoop. III / Jürgen Rooste

Index Scriptorium Estoniae

Rooste, Jürgen, 1979-

2009-01-01

Ülevaade järgmistest luuleraamatutest: Anmann, Aarne. Südametunnistuse mälestuseks. Tartu : A. Anmann, 2009 ; Ilmet, Peep. Meilmail. Tallinn : Varrak, 2009 ; Kasemaa, Andrus. Lagunemine. Tallinn : Eesti Keele Sihtasutus, 2009 ; Kuus, Anti ; Oll, Sulev. Öö mõte on kuus. Tallinn : Akta A. K., 2008 ; Meres, Triinu. Lagunemine. Tartu : Hermes, 2009 ; Tasuja, Triin. Provintsiluule. Tartu : Värske Rõhk, 2009

Magnesium and Space Flight

Science.gov (United States)

Smith, Scott M.; Zwart, Sara R.

2015-01-01

Magnesium is an essential nutrient for muscle, cardiovascular, and bone health on Earth, and during space flight. We sought to evaluate magnesium status in 43 astronauts (34 male, 9 female; 47 ± 5 years old, mean ± SD) before, during, and after 4–6-month space missions. We also studied individuals participating in a ground analog of space flight (head-down-tilt bed rest; n = 27 (17 male, 10 female), 35 ± 7 years old). We evaluated serum concentration and 24-h urinary excretion of magnesium, along with estimates of tissue magnesium status from sublingual cells. Serum magnesium increased late in flight, while urinary magnesium excretion was higher over the course of 180-day space missions. Urinary magnesium increased during flight but decreased significantly at landing. Neither serum nor urinary magnesium changed during bed rest. For flight and bed rest, significant correlations existed between the area under the curve of serum and urinary magnesium and the change in total body bone mineral content. Tissue magnesium concentration was unchanged after flight and bed rest. Increased excretion of magnesium is likely partially from bone and partially from diet, but importantly, it does not come at the expense of muscle tissue stores. While further study is needed to better understand the implications of these findings for longer space exploration missions, magnesium homeostasis and tissue status seem well maintained during 4–6-month space missions. PMID:26670248

Magnesium and Space Flight

Directory of Open Access Journals (Sweden)

Scott M. Smith

2015-12-01

Full Text Available Magnesium is an essential nutrient for muscle, cardiovascular, and bone health on Earth, and during space flight. We sought to evaluate magnesium status in 43 astronauts (34 male, 9 female; 47 ± 5 years old, mean ± SD before, during, and after 4–6-month space missions. We also studied individuals participating in a ground analog of space flight (head-down-tilt bed rest; n = 27 (17 male, 10 female, 35 ± 7 years old. We evaluated serum concentration and 24-h urinary excretion of magnesium, along with estimates of tissue magnesium status from sublingual cells. Serum magnesium increased late in flight, while urinary magnesium excretion was higher over the course of 180-day space missions. Urinary magnesium increased during flight but decreased significantly at landing. Neither serum nor urinary magnesium changed during bed rest. For flight and bed rest, significant correlations existed between the area under the curve of serum and urinary magnesium and the change in total body bone mineral content. Tissue magnesium concentration was unchanged after flight and bed rest. Increased excretion of magnesium is likely partially from bone and partially from diet, but importantly, it does not come at the expense of muscle tissue stores. While further study is needed to better understand the implications of these findings for longer space exploration missions, magnesium homeostasis and tissue status seem well maintained during 4–6-month space missions.

Flight Technical Error Analysis of the SATS Higher Volume Operations Simulation and Flight Experiments

Science.gov (United States)

Williams, Daniel M.; Consiglio, Maria C.; Murdoch, Jennifer L.; Adams, Catherine H.

2005-01-01

This paper provides an analysis of Flight Technical Error (FTE) from recent SATS experiments, called the Higher Volume Operations (HVO) Simulation and Flight experiments, which NASA conducted to determine pilot acceptability of the HVO concept for normal operating conditions. Reported are FTE results from simulation and flight experiment data indicating the SATS HVO concept is viable and acceptable to low-time instrument rated pilots when compared with today s system (baseline). Described is the comparative FTE analysis of lateral, vertical, and airspeed deviations from the baseline and SATS HVO experimental flight procedures. Based on FTE analysis, all evaluation subjects, low-time instrument-rated pilots, flew the HVO procedures safely and proficiently in comparison to today s system. In all cases, the results of the flight experiment validated the results of the simulation experiment and confirm the utility of the simulation platform for comparative Human in the Loop (HITL) studies of SATS HVO and Baseline operations.

Doppler Broadening of In-Flight Positron Annihilation Radiation due to Electron Momentum

International Nuclear Information System (INIS)

Hunt, A. W.; Cassidy, D. B.; Sterne, P. A.; Cowan, T. E.; Howell, R. H.; Lynn, K. G.; Golevchenko, J. A.

2001-01-01

We report the first observation of electron momentum contributions to the Doppler broadening of radiation produced by in-flight two-photon annihilation in solids. In these experiments an approximately 2.5 MeV positron beam impinged on thin polyethylene, aluminum, and gold targets. Since energetic positrons easily penetrate the nuclear Coulomb potential and do not cause a strong charge polarization, the experimental annihilation line shapes agree well with calculations based on a simple independent-particle model. Moreover, annihilations with the deepest core electrons are greatly enhanced

Advanced in-flight measurement techniques

CERN Document Server

Lawson, Nicholas; Jentink, Henk; Kompenhans, Jürgen

2013-01-01

The book presents a synopsis of the main results achieved during the 3 year EU-project "Advanced Inflight Measurement Techniques (AIM)" which applied advanced image based measurement techniques to industrial flight testing. The book is intended to be not only an overview on the AIM activities but also a guide on the application of advanced optical measurement techniques for future flight testing. Furthermore it is a useful guide for engineers in the field of experimental methods and flight testing who face the challenge of a future requirement for the development of highly accurate non-intrusive in-flight measurement techniques.

Armstrong Flight Research Center Flight Test Capabilities and Opportunities for the Applications of Wireless Data Acquisition Systems

Science.gov (United States)

Hang, Richard

2015-01-01

The presentation will overview NASA Armstrong Flight Research Centers flight test capabilities, which can provide various means for flight testing of passive and active wireless sensor systems, also, it will address the needs of the wireless data acquisition solutions for the centers flight instrumentation issues such as additional weight caused by added instrumentation wire bundles, connectors, wire cables routing, moving components, etc., that the Passive Wireless Sensor Technology Workshop may help. The presentation shows the constraints and requirements that the wireless sensor systems will face in the flight test applications.

Flight demonstration of flight termination system and solid rocket motor ignition using semiconductor laser initiated ordnance

Science.gov (United States)

Schulze, Norman R.; Maxfield, B.; Boucher, C.

1995-01-01

Solid State Laser Initiated Ordnance (LIO) offers new technology having potential for enhanced safety, reduced costs, and improved operational efficiency. Concerns over the absence of programmatic applications of the technology, which has prevented acceptance by flight programs, should be abated since LIO has now been operationally implemented by the Laser Initiated Ordnance Sounding Rocket Demonstration (LOSRD) Program. The first launch of solid state laser diode LIO at the NASA Wallops Flight Facility (WFF) occurred on March 15, 1995 with all mission objectives accomplished. This project, Phase 3 of a series of three NASA Headquarters LIO demonstration initiatives, accomplished its objective by the flight of a dedicated, all-LIO sounding rocket mission using a two-stage Nike-Orion launch vehicle. LIO flight hardware, made by The Ensign-Bickford Company under NASA's first Cooperative Agreement with Profit Making Organizations, safely initiated three demanding pyrotechnic sequence events, namely, solid rocket motor ignition from the ground and in flight, and flight termination, i.e., as a Flight Termination System (FTS). A flight LIO system was designed, built, tested, and flown to support the objectives of quickly and inexpensively putting LIO through ground and flight operational paces. The hardware was fully qualified for this mission, including component testing as well as a full-scale system test. The launch accomplished all mission objectives in less than 11 months from proposal receipt. This paper concentrates on accomplishments of the ordnance aspects of the program and on the program's implementation and results. While this program does not generically qualify LIO for all applications, it demonstrated the safety, technical, and operational feasibility of those two most demanding applications, using an all solid state safe and arm system in critical flight applications.

A Data Filter for Identifying Steady-State Operating Points in Engine Flight Data for Condition Monitoring Applications

Science.gov (United States)

Simon, Donald L.; Litt, Jonathan S.

2010-01-01

This paper presents an algorithm that automatically identifies and extracts steady-state engine operating points from engine flight data. It calculates the mean and standard deviation of select parameters contained in the incoming flight data stream. If the standard deviation of the data falls below defined constraints, the engine is assumed to be at a steady-state operating point, and the mean measurement data at that point are archived for subsequent condition monitoring purposes. The fundamental design of the steady-state data filter is completely generic and applicable for any dynamic system. Additional domain-specific logic constraints are applied to reduce data outliers and variance within the collected steady-state data. The filter is designed for on-line real-time processing of streaming data as opposed to post-processing of the data in batch mode. Results of applying the steady-state data filter to recorded helicopter engine flight data are shown, demonstrating its utility for engine condition monitoring applications.

Theseus First Flight - May 24, 1996

Science.gov (United States)

1996-01-01

The Theseus prototype research aircraft shows off its high aspect-ratio wing as it lifts off from Rogers Dry Lake during its first test flight from NASA's Dryden Flight Research Center, Edwards, California, on May 24, 1996. The Theseus aircraft, built and operated by Aurora Flight Sciences Corporation, Manassas, Virginia, was a unique aircraft flown at NASA's Dryden Flight Research Center, Edwards, California, under a cooperative agreement between NASA and Aurora. Dryden hosted the Theseus program, providing hangar space and range safety for flight testing. Aurora Flight Sciences was responsible for the actual flight testing, vehicle flight safety, and operation of the aircraft. The Theseus remotely piloted aircraft flew its maiden flight on May 24, 1996, at Dryden. During its sixth flight on November 12, 1996, Theseus experienced an in-flight structural failure that resulted in the loss of the aircraft. As of the beginning of the year 2000, Aurora had not rebuilt the aircraft. Theseus was built for NASA under an innovative, $4.9 million fixed-price contract by Aurora Flight Sciences Corporation and its partners, West Virginia University, Morgantown, West Virginia, and Fairmont State College, Fairmont, West Virginia. The twin-engine, unpiloted vehicle had a 140-foot wingspan, and was constructed largely of composite materials. Powered by two 80-horsepower, turbocharged piston engines that drove twin 9-foot-diameter propellers, Theseus was designed to fly autonomously at high altitudes, with takeoff and landing under the active control of a ground-based pilot in a ground control station 'cockpit.' With the potential ability to carry 700 pounds of science instruments to altitudes above 60,000 feet for durations of greater than 24 hours, Theseus was intended to support research in areas such as stratospheric ozone depletion and the atmospheric effects of future high-speed civil transport aircraft engines. Instruments carried aboard Theseus also would be able to

Altitude exposures during commercial flight: a reappraisal.

Science.gov (United States)

Hampson, Neil B; Kregenow, David A; Mahoney, Anne M; Kirtland, Steven H; Horan, Kathleen L; Holm, James R; Gerbino, Anthony J

2013-01-01

Hypobaric hypoxia during commercial air travel has the potential to cause or worsen hypoxemia in individuals with pre-existing cardiopulmonary compromise. Knowledge of cabin altitude pressures aboard contemporary flights is essential to counseling patients accurately about flying safety. The objective of the study was to measure peak cabin altitudes during U.S. domestic commercial flights on a variety of aircraft. A handheld mountaineering altimeter was carried by the investigators in the plane cabin during commercial air travel and peak cabin altitude measured. The values were then compared between aircraft models, aircraft classes, and distances flown. The average peak cabin altitude on 207 flights aboard 17 different aircraft was 6341 +/- 1813 ft (1933 m +/- 553 m), significantly higher than when measured in a similar fashion in 1988. Peak cabin altitude was significantly higher for flights longer than 750 mi (7085 +/- 801 ft) compared to shorter flights (5160 +/- 2290 ft/1573 +/- 698 m). Cabin altitude increased linearly with flight distance for flights up to 750 mi in length, but was independent of flight distance for flights exceeding 750 mi. Peak cabin altitude was less than 5000 ft (1524 m) in 70% of flights shorter than 500 mi. Peak cabin altitudes greater than 8000 ft (2438 m) were measured on approximately 10% of the total flights. Peak cabin altitude on commercial aircraft flights has risen over time. Cabin altitude is lower with flights of shorter distance. Physicians should take these factors into account when determining an individual's need for supplemental oxygen during commercial air travel.

Poor flight performance in deep-diving cormorants.

Science.gov (United States)

Watanabe, Yuuki Y; Takahashi, Akinori; Sato, Katsufumi; Viviant, Morgane; Bost, Charles-André

2011-02-01

Aerial flight and breath-hold diving present conflicting morphological and physiological demands, and hence diving seabirds capable of flight are expected to face evolutionary trade-offs regarding locomotory performances. We tested whether Kerguelen shags Phalacrocorax verrucosus, which are remarkable divers, have poor flight capability using newly developed tags that recorded their flight air speed (the first direct measurement for wild birds) with propeller sensors, flight duration, GPS position and depth during foraging trips. Flight air speed (mean 12.7 m s(-1)) was close to the speed that minimizes power requirement, rather than energy expenditure per distance, when existing aerodynamic models were applied. Flights were short (mean 92 s), with a mean summed duration of only 24 min day(-1). Shags sometimes stayed at the sea surface without diving between flights, even on the way back to the colony, and surface durations increased with the preceding flight durations; these observations suggest that shags rested after flights. Our results indicate that their flight performance is physiologically limited, presumably compromised by their great diving capability (max. depth 94 m, duration 306 s) through their morphological adaptations for diving, including large body mass (enabling a large oxygen store), small flight muscles (to allow for large leg muscles for underwater propulsion) and short wings (to decrease air volume in the feathers and hence buoyancy). The compromise between flight and diving, as well as the local bathymetry, shape the three-dimensional foraging range (<26 km horizontally, <94 m vertically) in this bottom-feeding cormorant.

Muulane või surmasõlm / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

2007-01-01

Tutvustus: Ivinskaja, Olga. Aastad Boriss Pasternakiga, ehk, Aja vangis / tlk. Vilma Matsov. Tallinn : Varrak, 2006 ; Baranov, Vadim. Maksim Gorki. Elu ja surma saladus / tlk. Jüri Pärni. Tallinn : Kunst, 2006 ; Troyat, Henri. Aleksander III : lumetsaar / tlk. Jana Porila. Tallinn : Eesti Raamat, 2006 ; Runnel, Hando. Viru veri ei värise. [Tartu] : Ilmamaa, 2006 ; Pärnik, Ylo M. Dr. Julius von Scultz-Bertram. Tartu : Ilmamaa, 2006

Development and Flight Test of an Augmented Thrust-Only Flight Control System on an MD-11 Transport Airplane

Science.gov (United States)

Burcham, Frank W., Jr.; Maine, Trindel A.; Burken, John J.; Pappas, Drew

1996-01-01

An emergency flight control system using only engine thrust, called Propulsion-Controlled Aircraft (PCA), has been developed and flight tested on an MD-11 airplane. In this thrust-only control system, pilot flight path and track commands and aircraft feedback parameters are used to control the throttles. The PCA system was installed on the MD-11 airplane using software modifications to existing computers. Flight test results show that the PCA system can be used to fly to an airport and safely land a transport airplane with an inoperative flight control system. In up-and-away operation, the PCA system served as an acceptable autopilot capable of extended flight over a range of speeds and altitudes. The PCA approaches, go-arounds, and three landings without the use of any non-nal flight controls have been demonstrated, including instrument landing system-coupled hands-off landings. The PCA operation was used to recover from an upset condition. In addition, PCA was tested at altitude with all three hydraulic systems turned off. This paper reviews the principles of throttles-only flight control; describes the MD-11 airplane and systems; and discusses PCA system development, operation, flight testing, and pilot comments.

Optimal pitching axis location of flapping wings for efficient hovering flight.

Science.gov (United States)

Wang, Q; Goosen, J F L; van Keulen, F

2017-09-01

Flapping wings can pitch passively about their pitching axes due to their flexibility, inertia, and aerodynamic loads. A shift in the pitching axis location can dynamically alter the aerodynamic loads, which in turn changes the passive pitching motion and the flight efficiency. Therefore, it is of great interest to investigate the optimal pitching axis for flapping wings to maximize the power efficiency during hovering flight. In this study, flapping wings are modeled as rigid plates with non-uniform mass distribution. The wing flexibility is represented by a linearly torsional spring at the wing root. A predictive quasi-steady aerodynamic model is used to evaluate the lift generated by such wings. Two extreme power consumption scenarios are modeled for hovering flight, i.e. the power consumed by a drive system with and without the capacity of kinetic energy recovery. For wings with different shapes, the optimal pitching axis location is found such that the cycle-averaged power consumption during hovering flight is minimized. Optimization results show that the optimal pitching axis is located between the leading edge and the mid-chord line, which shows close resemblance to insect wings. An optimal pitching axis can save up to 33% of power during hovering flight when compared to traditional wings used by most of flapping wing micro air vehicles (FWMAVs). Traditional wings typically use the straight leading edge as the pitching axis. With the optimized pitching axis, flapping wings show higher pitching amplitudes and start the pitching reversals in advance of the sweeping reversals. These phenomena lead to higher lift-to-drag ratios and, thus, explain the lower power consumption. In addition, the optimized pitching axis provides the drive system higher potential to recycle energy during the deceleration phases as compared to their counterparts. This observation underlines the particular importance of the wing pitching axis location for energy-efficient FWMAVs when

Modelling the line shape of very low energy peaks of positron beam induced secondary electrons measured using a time of flight spectrometer

International Nuclear Information System (INIS)

Fairchild, A J; Chirayath, V A; Gladen, R W; Chrysler, M D; Koymen, A R; Weiss, A H

2017-01-01

In this paper, we present results of numerical modelling of the University of Texas at Arlington’s time of flight positron annihilation induced Auger electron spectrometer (UTA TOF-PAES) using SIMION® 8.1 Ion and Electron Optics Simulator. The time of flight (TOF) spectrometer measures the energy of electrons emitted from the surface of a sample as a result of the interaction of low energy positrons with the sample surface. We have used SIMION® 8.1 to calculate the times of flight spectra of electrons leaving the sample surface with energies and angles dispersed according to distribution functions chosen to model the positron induced electron emission process and have thus obtained an estimate of the true electron energy distribution. The simulated TOF distribution was convolved with a Gaussian timing resolution function and compared to the experimental distribution. The broadening observed in the simulated TOF spectra was found to be consistent with that observed in the experimental secondary electron spectra of Cu generated as a result of positrons incident with energy 1.5 eV to 901 eV, when a timing resolution of 2.3 ns was assumed. (paper)

Nutritional Biochemistry of Space Flight

Science.gov (United States)

Smith, Scott M.

2000-01-01

Adequate nutrition is critical for maintenance of crew health during and after extended-duration space flight. The impact of weightlessness on human physiology is profound, with effects on many systems related to nutrition, including bone, muscle, hematology, fluid and electrolyte regulation. Additionally, we have much to learn regarding the impact of weightlessness on absorption, mtabolism , and excretion of nutrients, and this will ultimately determine the nutrient requirements for extended-duration space flight. Existing nutritional requirements for extended-duration space flight have been formulated based on limited flight research, and extrapolation from ground-based research. NASA's Nutritional Biochemistry Laboratory is charged with defining the nutritional requirements for space flight. This is accomplished through both operational and research projects. A nutritional status assessment program is included operationally for all International Space Station astronauts. This medical requirement includes biochemical and dietary assessments, and is completed before, during, and after the missions. This program will provide information about crew health and nutritional status, and will also provide assessments of countermeasure efficacy. Ongoing research projects include studies of calcium and bone metabolism, and iron absorption and metabolism. The calcium studies include measurements of endocrine regulation of calcium homeostasis, biochemical marker of bone metabolism, and tracer kinetic studies of calcium movement in the body. These calcium kinetic studies allow for estimation of intestinal absorption, urinary excretion, and perhaps most importantly - deposition and resorption of calcium from bone. The Calcium Kinetics experiment is currently being prepared for flight on the Space Shuttle in 2001, and potentially for subsequent Shuttle and International Space Station missions. The iron study is intended to assess whether iron absorption is down-regulated dUl1ng

In-flight Fault Detection and Isolation in Aircraft Flight Control Systems

Science.gov (United States)

Azam, Mohammad; Pattipati, Krishna; Allanach, Jeffrey; Poll, Scott; Patterson-Hine, Ann

2005-01-01

In this paper we consider the problem of test design for real-time fault detection and isolation (FDI) in the flight control system of fixed-wing aircraft. We focus on the faults that are manifested in the control surface elements (e.g., aileron, elevator, rudder and stabilizer) of an aircraft. For demonstration purposes, we restrict our focus on the faults belonging to nine basic fault classes. The diagnostic tests are performed on the features extracted from fifty monitored system parameters. The proposed tests are able to uniquely isolate each of the faults at almost all severity levels. A neural network-based flight control simulator, FLTZ(Registered TradeMark), is used for the simulation of various faults in fixed-wing aircraft flight control systems for the purpose of FDI.

Neon-like Iron Ion Lines Measured in NIFS/Large Helical Device (LHD) and Hinode/EUV Imaging Spectrometer (EIS)

Science.gov (United States)

Watanabe, Tetsuya; Hara, Hirohisa; Murakami, Izumi; Kato, Daiji; Sakaue, Hiroyuki A.; Morita, Shigeru; Suzuki, Chihiro; Tamura, Naoki; Yamamoto, Norimasa; Nakamura, Nobuyuki

2017-06-01

Line intensities emerging from the Ne-sequence iron ion (Fe XVII) are measured in the laboratory, by the Large Helical Device at the National Institute for Fusion Science, and in the solar corona by the EUV Imaging Spectrometer (EIS) on board the Hinode mission. The intensity ratios of Fe XVII λ 204.6/λ 254.8 are derived in the laboratory by unblending the contributions of the Fe XIII and XII line intensities. They are consistent with theoretical predictions and solar observations, the latter of which endorses the in-flight radiometric calibrations of the EIS instrument. The still remaining temperature-dependent behavior of the line ratio suggests the contamination of lower-temperature iron lines that are blended with the λ 204.6 line.

Neon-like Iron Ion Lines Measured in NIFS/Large Helical Device (LHD) and Hinode /EUV Imaging Spectrometer (EIS)

Energy Technology Data Exchange (ETDEWEB)

Watanabe, Tetsuya; Hara, Hirohisa [National Astronomical Observatory, National Institutes of Natural Sciences 2-21-1 Osawa Mitaka Tokyo, 181-8588 (Japan); Murakami, Izumi; Kato, Daiji; Morita, Shigeru [SOKENDAI (Graduate University for Advanced Studies) Hayama, Miura-gun, Kanagawa, 240-0193 (Japan); Sakaue, Hiroyuki A.; Suzuki, Chihiro; Tamura, Naoki [National Institute for Fusion Science, National Institutes of Natural Sciences 322-6 Oroshi-cho, Toki Gifu, 509-5292 (Japan); Yamamoto, Norimasa [Chubu University 1200 Matsumoto-cho, Kasugai Aichi, 487-0027 (Japan); Nakamura, Nobuyuki, E-mail: watanabe@uvlab.mtk.nao.ac.jp [The University of Electro-Communications 1-5-1 Chofugaoka, Chofu Tokyo, 182-8585 (Japan)

2017-06-10

Line intensities emerging from the Ne-sequence iron ion (Fe xvii) are measured in the laboratory, by the Large Helical Device at the National Institute for Fusion Science, and in the solar corona by the EUV Imaging Spectrometer (EIS) on board the Hinode mission. The intensity ratios of Fe xvii λ 204.6/ λ 254.8 are derived in the laboratory by unblending the contributions of the Fe xiii and xii line intensities. They are consistent with theoretical predictions and solar observations, the latter of which endorses the in-flight radiometric calibrations of the EIS instrument. The still remaining temperature-dependent behavior of the line ratio suggests the contamination of lower-temperature iron lines that are blended with the λ 204.6 line.

Development and flight test of metal-lined CFRP cryogenic tank for reusable rocket

Science.gov (United States)

Higuchi, Ken; Takeuchi, Shinsuke; Sato, Eiichi; Naruo, Yoshihiro; Inatani, Yoshifumi; Namiki, Fumiharu; Tanaka, Kohtaro; Watabe, Yoko

2005-07-01

A cryogenic tank made of carbon fiber reinforced plastic (CFRP) shell with aluminum thin liner has been designed as a liquid hydrogen (LH2) tank for an ISAS reusable launch vehicle, and the function of it has been proven by repeated flights onboard the test vehicle called reusable vehicle testing (RVT) in October 2003. The liquid hydrogen tank has to be a pressure vessel, because the fuel of the engine of the test vehicle is supplied by fuel pressure. The pressure vessel of a combination of the outer shell of CFRP for strength element at a cryogenic temperature and the inner liner of aluminum for gas barrier has shown excellent weight merit for this purpose. Interfaces such as tank outline shape, bulk capacity, maximum expected operating pressure (MEOP), thermal insulation, pipe arrangement, and measurement of data are also designed to be ready onboard. This research has many aims, not only development of reusable cryogenic composite tank but also the demonstration of repeated operation including thermal cycle and stress cycle, familiarization with test techniques of operation of cryogenic composite tanks, and the accumulation of data for future design of tanks, vehicle structures, safety evaluation, and total operation systems.

International study of risk-mitigating factors and in-flight allergic reactions to peanut and tree nut.

Science.gov (United States)

Greenhawt, Matthew; MacGillivray, Fiona; Batty, Geraldine; Said, Maria; Weiss, Christopher

2013-03-01

Three studies have analyzed in-flight peanut/tree nut reactions, although the studies were conducted exclusively among Americans. We studied the international in-flight experience and determined the efficacy of certain risk-mitigation strategies. A 47-question on-line survey was distributed through the websites and social media outlets of the member organizations of the Food Allergy & Anaphylaxis Alliance. Both persons reporting an in-flight reaction and nonreactors were surveyed to assess details of air travel preparation and any reported reaction. Data were analyzed to determine the association among flying behaviors, reported reactions, and nationality. We found that 349 reactions were reported among 3273 respondents from 11 countries; 13.3% received epinephrine as treatment. Flight crews were notified about 50.1% of reactions. Sixty-nine percent of all respondents reported making a preflight accommodation request, although just 55% of reactors did so compared with 71.6% of nonreactors (P airline pillows or blankets, requested a buffer zone, requested other passengers not consume peanut/tree nut-containing products, or reported not consuming airline-provided food had significantly lower adjusted odds of reporting a reaction. In-flight peanut and tree nut reactions occur internationally. Epinephrine was sparsely used to treat reactions. We identified 8 risk-mitigating behaviors associated with lower odds of a reported reaction. Future study is necessary to further validate the effectiveness of these passenger-initiated risk-mitigating behaviors. Copyright © 2013 American Academy of Allergy, Asthma & Immunology. Published by Elsevier Inc. All rights reserved.

Digital virtual flight testing and evaluation method for flight characteristics airworthiness compliance of civil aircraft based on HQRM

Directory of Open Access Journals (Sweden)

Fan Liu

2015-02-01

Full Text Available In order to incorporate airworthiness requirements for flight characteristics into the entire development cycle of electronic flight control system (EFCS equipped civil aircraft, digital virtual flight testing and evaluation method based on handling qualities rating method (HQRM is proposed. First, according to HQRM, flight characteristics airworthiness requirements of civil aircraft in EFCS failure states are determined. On this basis, digital virtual flight testing model, comprising flight task digitized model, pilot controlling model, aircraft motion and atmospheric turbulence model, is used to simulate the realistic process of a pilot controlling an airplane to perform assigned flight tasks. According to the simulation results, flight characteristics airworthiness compliance of the airplane can be evaluated relying on the relevant regulations for handling qualities (HQ rating. Finally, this method is applied to a type of passenger airplane in a typical EFCS failure state, and preliminary conclusions concerning airworthiness compliance are derived quickly. The research results of this manuscript can provide important theoretical reference for EFCS design and actual airworthiness compliance verification of civil aircraft.

Supersonic Retropropulsion Flight Test Concepts

Science.gov (United States)

Post, Ethan A.; Dupzyk, Ian C.; Korzun, Ashley M.; Dyakonov, Artem A.; Tanimoto, Rebekah L.; Edquist, Karl T.

2011-01-01

NASA's Exploration Technology Development and Demonstration Program has proposed plans for a series of three sub-scale flight tests at Earth for supersonic retropropulsion, a candidate decelerator technology for future, high-mass Mars missions. The first flight test in this series is intended to be a proof-of-concept test, demonstrating successful initiation and operation of supersonic retropropulsion at conditions that replicate the relevant physics of the aerodynamic-propulsive interactions expected in flight. Five sub-scale flight test article concepts, each designed for launch on sounding rockets, have been developed in consideration of this proof-of-concept flight test. Commercial, off-the-shelf components are utilized as much as possible in each concept. The design merits of the concepts are compared along with their predicted performance for a baseline trajectory. The results of a packaging study and performance-based trade studies indicate that a sounding rocket is a viable launch platform for this proof-of-concept test of supersonic retropropulsion.

14 CFR 91.1061 - Augmented flight crews.

Science.gov (United States)

2010-01-01

...) Minimum After Duty Rest Period for Multi-Time Zone Flights 18 hours 24 hours ...) AIR TRAFFIC AND GENERAL OPERATING RULES GENERAL OPERATING AND FLIGHT RULES Fractional Ownership... crewmember, and no flight crewmember may accept an assignment, for flight time as a member of an augmented...

Time-of-flight data acquisition unit (DAU) for neutron scattering experiments. Specification of the requirements and design concept. Version 3.1

International Nuclear Information System (INIS)

Herdam, G.; Klessmann, H.; Wawer, W.; Adebayo, J.; David, G.; Szatmari, F.

1989-12-01

This specification describes the requirements for the Data Acquisition Unit (DAU) and defines the design concept for the functional units involved. The Data Acquisition Unit will be used in the following neutron scattering experiments: Time-of-Flight Spectrometer NEAT, Time-of-Flight Spectrometer SPAN. In addition, the data of the SPAN spectrometer in Spin Echo experiments will be accumulated. The Data Acquisition Unit can be characterised by the following requirements: Time-of-flight measurement with high time resolution (125 ns), sorting the time-of-flight in up to 4096 time channels (channel width ≥ 1 μs), selection of different time channel widths for peak and background, on-line time-of-flight correction for neutron flight paths of different lengths, sorting the detector position information in up to 4096 position channels, accumulation of two-dimensional spectra in a 32 Mbyte RAM memory (4 K time channels*4 K position channels*16 bits). Because of the stringent timing requirements the functional units of the DAU are hardware controlled via tables. The DAU is part of a process control system which has access to the functional units via the VMEbus in order to initialise, to load tables and control information, and to read status information and spectra. (orig.) With 18 figs

Getting started with Twitter Flight

CERN Document Server

Hamshere, Tom

2013-01-01

Getting Started with Twitter Flight is written with the intention to educate the readers, helping them learn how to build modular powerful applications with Flight, Twitter's cutting-edge JavaScript framework.This book is for anyone with a foundation in JavaScript who wants to build web applications. Flight is quick and easy to learn, built on technologies you already understand such as the DOM, events, and jQuery.

Metabolism during flight in two species of bats, Phyllostomus hastatus and Pteropus gouldii.

Science.gov (United States)

Thomas, S P

1975-08-01

The energetic cost of flight in a wind-tunnel was measured at various combinations of speed and flight angle from two species of bats whose body masses differ by almost an order of magnitude. The highest mean metabolic rate per unit body mass measured from P. hastatus (mean body mass, 0.093 kg) was 130.4 Wkg-1, and that for P. gouldii (mean body mass, 0.78 kg) was 69.6 Wkg-1. These highest metabolic rates, recorded from flying bats, are essentially the same as those predicted for flying birds of the same body masses, but are from 2.5 to 3.0 times greater than the highest metabolic rates of which similar-size exercising terrestrial mammals appear capable. The lowest mean rate of energy utilization per unit body mass P. hastatus required to sustain level flight was 94.2 Wkg-1 and that for P. gouldii was 53.4 Wkg-1. These data from flying bats together with comparable data for flying birds all fall along a straight line when plotted on double logarithmic coordinates as a function of body mass. Such data show that even the lowest metabolic requirements of bats and birds during level flight are about twice the highest metabolic capabilities of similar-size terrestrial mammals. Flying bats share with flying birds the ability to move substantially greater distance per unit energy consumed than walking or running mammals. Calculations show that P. hastatus requires only one-sixth the energy to cover a given distance as does the same-size terrestrial mammal, while P. gouldii requires one-fourth the energy of the same-size terrestrial mammal. An empirically derived equation is presented which enables one to make estimates of the metabolic rates of bats and birds during level flight in nature from body mass data alone. Metabolic data obtained in this study are compared with predictions calculated from an avian flight theory.

Flight telerobotic servicer legacy

Science.gov (United States)

Shattuck, Paul L.; Lowrie, James W.

1992-11-01

The Flight Telerobotic Servicer (FTS) was developed to enhance and provide a safe alternative to human presence in space. The first step for this system was a precursor development test flight (DTF-1) on the Space Shuttle. DTF-1 was to be a pathfinder for manned flight safety of robotic systems. The broad objectives of this mission were three-fold: flight validation of telerobotic manipulator (design, control algorithms, man/machine interfaces, safety); demonstration of dexterous manipulator capabilities on specific building block tasks; and correlation of manipulator performance in space with ground predictions. The DTF-1 system is comprised of a payload bay element (7-DOF manipulator with controllers, end-of-arm gripper and camera, telerobot body with head cameras and electronics module, task panel, and MPESS truss) and an aft flight deck element (force-reflecting hand controller, crew restraint, command and display panel and monitors). The approach used to develop the DTF-1 hardware, software and operations involved flight qualification of components from commercial, military, space, and R controller, end-of-arm tooling, force/torque transducer) and the development of the telerobotic system for space applications. The system is capable of teleoperation and autonomous control (advances state of the art); reliable (two-fault tolerance); and safe (man-rated). Benefits from the development flight included space validation of critical telerobotic technologies and resolution of significant safety issues relating to telerobotic operations in the Shuttle bay or in the vicinity of other space assets. This paper discusses the lessons learned and technology evolution that stemmed from developing and integrating a dexterous robot into a manned system, the Space Shuttle. Particular emphasis is placed on the safety and reliability requirements for a man-rated system as these are the critical factors which drive the overall system architecture. Other topics focused on include

Microgravity Flight - Accommodating Non-Human Primates

Science.gov (United States)

Dalton, Bonnie P.; Searby, Nancy; Ostrach, Louis

1994-01-01

Spacelab Life Sciences-3 (SLS-3) was scheduled to be the first United States man-tended microgravity flight containing Rhesus monkeys. The goal of this flight as in the five untended Russian COSMOS Bion flights and an earlier American Biosatellite flight, was to understand the biomedical and biological effects of a microgravity environment using the non-human primate as human surrogate. The SLS-3/Rhesus Project and COSMOS Primate-BIOS flights all utilized the rhesus monkey, Macaca mulatta. The ultimate objective of all flights with an animal surrogate has been to evaluate and understand biological mechanisms at both the system and cellular level, thus enabling rational effective countermeasures for future long duration human activity under microgravity conditions and enabling technical application to correction of common human physiological problems within earth's gravity, e.g., muscle strength and reloading, osteoporosis, immune deficiency diseases. Hardware developed for the SLS-3/Rhesus Project was the result of a joint effort with the French Centre National d'Etudes Spatiales (CNES) and the United States National Aeronautics and Space Administration (NASA) extending over the last decade. The flight hardware design and development required implementation of sufficient automation to insure flight crew and animal bio-isolation and maintenance with minimal impact to crew activities. A variety of hardware of varying functional capabilities was developed to support the scientific objectives of the original 22 combined French and American experiments, along with 5 Russian co-investigations, including musculoskeletal, metabolic, and behavioral studies. Unique elements of the Rhesus Research Facility (RRF) included separation of waste for daily delivery of urine and fecal samples for metabolic studies and a psychomotor test system for behavioral studies along with monitored food measurement. As in untended flights, telemetry measurements would allow monitoring of

Low Density Supersonic Decelerator Flight Dynamics Test-1 Flight Design and Targeting

Science.gov (United States)

Ivanov, Mark

2015-01-01

NASA's Low Density Supersonic Decelerator (LDSD) program was established to identify, develop, and eventually qualify to Test [i.e. Technology] Readiness Level (TRL) - 6 aerodynamic decelerators for eventual use on Mars. Through comprehensive Mars application studies, two distinct Supersonic Inflatable Aerodynamic Decelerator (SIAD) designs were chosen that afforded the optimum balance of benefit, cost, and development risk. In addition, a Supersonic Disk Sail (SSDS) parachute design was chosen that satisfied the same criteria. The final phase of the multi-tiered qualification process involves Earth Supersonic Flight Dynamics Tests (SFDTs) within environmental conditions similar to those that would be experienced during a Mars Entry, Descent, and Landing (EDL) mission. The first of these flight tests (i.e. SFDT-1) was completed on June 28, 2014 with two more tests scheduled for the summer of 2015 and 2016, respectively. The basic flight design for all the SFDT flights is for the SFDT test vehicle to be ferried to a float altitude of 120 kilo-feet by a 34 thousand cubic feet (Mcf) heavy lift helium balloon. Once float altitude is reached, the test vehicle is released from the balloon, spun-up for stability, and accelerated to supersonic speeds using a Star48 solid rocket motor. After burnout of the Star48 motor the vehicle decelerates to pre-flight selected test conditions for the deployment of the SIAD system. After further deceleration with the SIAD deployed, the SSDS parachute is then deployed stressing the performance of the parachute in the wake of the SIAD augmented blunt body. The test vehicle/SIAD/parachute system then descends to splashdown in the Pacific Ocean for eventual recovery. This paper will discuss the development of both the test vehicle and the trajectory sequence including design trade-offs resulting from the interaction of both engineering efforts. In addition, the SFDT-1 nominal trajectory design and associated sensitivities will be discussed

Aging Enhances Indirect Flight Muscle Fiber Performance yet Decreases Flight Ability in Drosophila

Energy Technology Data Exchange (ETDEWEB)

Miller, Mark S.; Lekkas, Panagiotis; Braddock, Joan M.; Farman, Gerrie P.; Ballif, Bryan A.; Irving, Thomas C.; Maughan, David W.; Vigoreaux, Jim O. (IIT); (Vermont)

2008-10-02

We investigated the effects of aging on Drosophila melanogaster indirect flight muscle from the whole organism to the actomyosin cross-bridge. Median-aged (49-day-old) flies were flight impaired, had normal myofilament number and packing, barely longer sarcomeres, and slight mitochondrial deterioration compared with young (3-day-old) flies. Old (56-day-old) flies were unable to beat their wings, had deteriorated ultrastructure with severe mitochondrial damage, and their skinned fibers failed to activate with calcium. Small-amplitude sinusoidal length perturbation analysis showed median-aged indirect flight muscle fibers developed greater than twice the isometric force and power output of young fibers, yet cross-bridge kinetics were similar. Large increases in elastic and viscous moduli amplitude under active, passive, and rigor conditions suggest that median-aged fibers become stiffer longitudinally. Small-angle x-ray diffraction indicates that myosin heads move increasingly toward the thin filament with age, accounting for the increased transverse stiffness via cross-bridge formation. We propose that the observed protein composition changes in the connecting filaments, which anchor the thick filaments to the Z-disk, produce compensatory increases in longitudinal stiffness, isometric tension, power and actomyosin interaction in aging indirect flight muscle. We also speculate that a lack of MgATP due to damaged mitochondria accounts for the decreased flight performance.

Ares I-X Flight Test Philosophy

Science.gov (United States)

Davis, S. R.; Tuma, M. L.; Heitzman, K.

2007-01-01

In response to the Vision for Space Exploration, the National Aeronautics and Space Administration (NASA) has defined a new space exploration architecture to return humans to the Moon and prepare for human exploration of Mars. One of the first new developments will be the Ares I Crew Launch Vehicle (CLV), which will carry the Orion Crew Exploration Vehicle (CEV), into Low Earth Orbit (LEO) to support International Space Station (ISS) missions and, later, support lunar missions. As part of Ares I development, NASA will perform a series of Ares I flight tests. The tests will provide data that will inform the engineering and design process and verify the flight hardware and software. The data gained from the flight tests will be used to certify the new Ares/Orion vehicle for human space flight. The primary objectives of this first flight test (Ares I-X) are the following: Demonstrate control of a dynamically similar integrated Ares CLV/Orion CEV using Ares CLV ascent control algorithms; Perform an in-flight separation/staging event between an Ares I-similar First Stage and a representative Upper Stage; Demonstrate assembly and recovery of a new Ares CLV-like First Stage element at Kennedy Space Center (KSC); Demonstrate First Stage separation sequencing, and quantify First Stage atmospheric entry dynamics and parachute performance; and Characterize the magnitude of the integrated vehicle roll torque throughout the First Stage (powered) flight. This paper will provide an overview of the Ares I-X flight test process and details of the individual flight tests.

Remote radio control of insect flight

Directory of Open Access Journals (Sweden)

Hirotaka Sato

2009-10-01

Full Text Available We demonstrated the remote control of insects in free flight via an implantable radio-equipped miniature neural stimulating system. The pronotum mounted system consisted of neural stimulators, muscular stimulators, a radio transceiver-equipped microcontroller and a microbattery. Flight initiation, cessation and elevation control were accomplished through neural stimulus of the brain which elicited, suppressed or modulated wing oscillation. Turns were triggered through the direct muscular stimulus of either of the basalar muscles. We characterized the response times, success rates, and free-flight trajectories elicited by our neural control systems in remotely-controlled beetles. We believe this type of technology will open the door to in-flight perturbation and recording of insect flight responses.

Remote radio control of insect flight.

Science.gov (United States)

Sato, Hirotaka; Berry, Christopher W; Peeri, Yoav; Baghoomian, Emen; Casey, Brendan E; Lavella, Gabriel; Vandenbrooks, John M; Harrison, Jon F; Maharbiz, Michel M

2009-01-01

We demonstrated the remote control of insects in free flight via an implantable radio-equipped miniature neural stimulating system. The pronotum mounted system consisted of neural stimulators, muscular stimulators, a radio transceiver-equipped microcontroller and a microbattery. Flight initiation, cessation and elevation control were accomplished through neural stimulus of the brain which elicited, suppressed or modulated wing oscillation. Turns were triggered through the direct muscular stimulus of either of the basalar muscles. We characterized the response times, success rates, and free-flight trajectories elicited by our neural control systems in remotely controlled beetles. We believe this type of technology will open the door to in-flight perturbation and recording of insect flight responses.

Twin City - past 1823-2013 : EHTE ja Haaga-Helia ühisprojekt / Tiit Kask, Ain Hinsberg

Index Scriptorium Estoniae

Kask, Tiit

2012-01-01

Turismikoolide ühisprojektist "Twin City - Empowering & Designing Twin-Capital Destination - Past, Present and Future of Tourism in Greater-Helsinki and Greater-Tallinn Area", mille eesmärgiks on Tallinna ja Helsingi kui ühtse turismisihtkoha käsitluse loomine ja 26. aprillil Tallinnas toimunud seminarist "TwinCity Helsinki-Tallinn / Tallinn & Estonian tourism 1813-2013", mis kutsus üles tähistama Tallinna (Kadrioru) merekuurordi ja "Eesti Turismimajandus 200" juubelit 2013. aastal

Flight Test Maneuvers for Efficient Aerodynamic Modeling

Science.gov (United States)

Morelli, Eugene A.

2011-01-01

Novel flight test maneuvers for efficient aerodynamic modeling were developed and demonstrated in flight. Orthogonal optimized multi-sine inputs were applied to aircraft control surfaces to excite aircraft dynamic response in all six degrees of freedom simultaneously while keeping the aircraft close to chosen reference flight conditions. Each maneuver was designed for a specific modeling task that cannot be adequately or efficiently accomplished using conventional flight test maneuvers. All of the new maneuvers were first described and explained, then demonstrated on a subscale jet transport aircraft in flight. Real-time and post-flight modeling results obtained using equation-error parameter estimation in the frequency domain were used to show the effectiveness and efficiency of the new maneuvers, as well as the quality of the aerodynamic models that can be identified from the resultant flight data.

Kolakowski : kaks vaatepunkti, kaks dialektikat / Andre Trinity

Index Scriptorium Estoniae

Trinity, André, pseud., 1974-

2004-01-01

Rets. rmt.: Kolakowski, Leszek. Horror metaphysicus. Tallinn, 2000 ; Kolakowski, Leszek. Religioon : Kui Jumalat ei ole olemas...Jumalast, kuradist, patust ja nn religioonifilosoofia teistest muredest. Tallinn, 2004

Raamatupärlid / Mihkel Mutt

Index Scriptorium Estoniae

Mutt, Mihkel, 1953-

2007-01-01

Tutvustus: Traat, Mats. Naised ja pojad ajakirjas Looming, nr. 2-5 ; Applebaum, Anne. Gulag. Tallinn : Varrak, 2005 ; Yourcenar, Marguerite. Silmapaistmatu inimene. Ilus hommik. Tallinn : Kultuurileht, 2006

Comparison of Commercial Aircraft Fuel Requirements in Regards to FAR, Flight Profile Simulation, and Flight Operational Techniques

Science.gov (United States)

Heitzman, Nicholas

There are significant fuel consumption consequences for non-optimal flight operations. This study is intended to analyze and highlight areas of interest that affect fuel consumption in typical flight operations. By gathering information from actual flight operators (pilots, dispatch, performance engineers, and air traffic controllers), real performance issues can be addressed and analyzed. A series of interviews were performed with various individuals in the industry and organizations. The wide range of insight directed this study to focus on FAA regulations, airline policy, the ATC system, weather, and flight planning. The goal is to highlight where operational performance differs from design intent in order to better connect optimization with actual flight operations. After further investigation and consensus from the experienced participants, the FAA regulations do not need any serious attention until newer technologies and capabilities are implemented. The ATC system is severely out of date and is one of the largest limiting factors in current flight operations. Although participants are pessimistic about its timely implementation, the FAA's NextGen program for a future National Airspace System should help improve the efficiency of flight operations. This includes situational awareness, weather monitoring, communication, information management, optimized routing, and cleaner flight profiles like Required Navigation Performance (RNP) and Continuous Descent Approach (CDA). Working off the interview results, trade-studies were performed using an in-house flight profile simulation of a Boeing 737-300, integrating NASA legacy codes EDET and NPSS with a custom written mission performance and point-performance "Skymap" calculator. From these trade-studies, it was found that certain flight conditions affect flight operations more than others. With weather, traffic, and unforeseeable risks, flight planning is still limited by its high level of precaution. From this

14 CFR 125.265 - Flight engineer requirements.

Science.gov (United States)

2010-01-01

... 14 Aeronautics and Space 3 2010-01-01 2010-01-01 false Flight engineer requirements. 125.265... Requirements § 125.265 Flight engineer requirements. (a) No person may operate an airplane for which a flight engineer is required by the type certification requirements without a flight crewmember holding a current...

Development and Flight Testing of a Neural Network Based Flight Control System on the NF-15B Aircraft

Science.gov (United States)

Bomben, Craig R.; Smolka, James W.; Bosworth, John T.; Silliams-Hayes, Peggy S.; Burken, John J.; Larson, Richard R.; Buschbacher, Mark J.; Maliska, Heather A.

2006-01-01

The Intelligent Flight Control System (IFCS) project at the NASA Dryden Flight Research Center, Edwards AFB, CA, has been investigating the use of neural network based adaptive control on a unique NF-15B test aircraft. The IFCS neural network is a software processor that stores measured aircraft response information to dynamically alter flight control gains. In 2006, the neural network was engaged and allowed to learn in real time to dynamically alter the aircraft handling qualities characteristics in the presence of actual aerodynamic failure conditions injected into the aircraft through the flight control system. The use of neural network and similar adaptive technologies in the design of highly fault and damage tolerant flight control systems shows promise in making future aircraft far more survivable than current technology allows. This paper will present the results of the IFCS flight test program conducted at the NASA Dryden Flight Research Center in 2006, with emphasis on challenges encountered and lessons learned.

14 CFR 63.42 - Flight engineer certificate issued on basis of a foreign flight engineer license.

Science.gov (United States)

2010-01-01

... section, may have a flight engineer certificate issued to him for the operation of civil aircraft of U.S... engineer certificate issued under this section may act as a flight engineer of a civil aircraft of U.S... 14 Aeronautics and Space 2 2010-01-01 2010-01-01 false Flight engineer certificate issued on basis...

14 CFR 91.1095 - Initial and transition training and checking: Flight instructors (aircraft), flight instructors...

Science.gov (United States)

2010-01-01

... instructor certificate— (i) The fundamental principles of the teaching-learning process; (ii) Teaching... Management § 91.1095 Initial and transition training and checking: Flight instructors (aircraft), flight...

Marguerite Duras ja tema võimukolmnurgad / Kärt Hellerma

Index Scriptorium Estoniae

Hellerma, Kärt, 1956-

2007-01-01

Arvustus: Duras, Marguerite. Armuke / tlk. Malle Talvet. Tallinn : Perioodika, 1989. (Loomingu Raamatukogu ; 1989, 11-12) ; Duras, Marguerite. Tamm Vaikse ookeani vastu / tlk. Triinu Tamm. Tallinn : Varrak, 2006

Forgotten Sunrise "Forgotten Sunrise. Behind The Abysmal Sky / Forever Sleeping Greystones". "The Moments When God Was Wrong" / Siim Nestor

Index Scriptorium Estoniae

Nestor, Siim, 1974-

2009-01-01

Arvustus: Forgotten Sunrise. Behind The Abysmal Sky / Forever Sleeping Greystones. [Tallinn] : Nailboard, 2009. Forgotten Sunrise. The Moments When God Was Wrong. [Tallinn] : Forgotten Sunrise, 2009. Uutest heliplaatidest

Uue oskuse võlu / Helen Talalaev

Index Scriptorium Estoniae

Talalaev, Helen

2009-01-01

Tutvustatakse kirjastuse TEA väljaantud õppekomplekte: Tomalin, Barry. Westminster English. Tallinn : TEA Kirjastus, 2009 ; Mangus, Inga. Vene keele õpik : algajale ja taasalustajale. Tallinn : TEA Kirjastus, 2008

Kolm debüüti / Jaak Urmet

Index Scriptorium Estoniae

Urmet, Jaak, 1979-

2001-01-01

Arvustus: Afanasjev, Vahur. Kandiline maailm. Tartu : Irboska Teataja Kirjastus, 2000 ; Ehin, Kristiina. Kevad Astrahanis : luuletusi 1992-1999. Tallinn : Huma, 2000 ; Kaldmaa, Jüri. Passioon. Tallinn : Huma, 2000

Kunst ja selle tegijad kuulugu rahvale / Stella Sägi

Index Scriptorium Estoniae

Sägi, Stella

2004-01-01

Kruus, Oskar. Kakskümmend üks pulma ja üksteist surma : kirjanduslooliste vestete kogumik. Tallinn : Faatum, 2003 ; Kruus, Oskar. Parunessi pihtimus : [biograafiline romaan]. Tallinn : Faatum, 2004

"Oh, homme on jälle kunst! Mida ma küll tunnis teen?" / Edna Vahter

Index Scriptorium Estoniae

Vahter, Edna

2002-01-01

Kunstiõpetusest alushariduses. Rmt. : Vahter, Edna. Kinnipüütud lehesadu : [kunstiõpetuse vihik]. - [Tallinn] : Avita, 2001; Vahter, Edna. Lumisem lumeaeg : [kunstiõpetuse vihik]. - [Tallinn] : Avita, 2001

Affordable Flight Demonstration of the GTX Air-Breathing SSTO Vehicle Concept

Science.gov (United States)

Krivanek, Thomas M.; Roche, Joseph M.; Riehl, John P.; Kosareo, Daniel N.

2003-01-01

The rocket based combined cycle (RBCC) powered single-stage-to-orbit (SSTO) reusable launch vehicle has the potential to significantly reduce the total cost per pound for orbital payload missions. To validate overall system performance, a flight demonstration must be performed. This paper presents an overview of the first phase of a flight demonstration program for the GTX SSTO vehicle concept. Phase 1 will validate the propulsion performance of the vehicle configuration over the supersonic and hypersonic air- breathing portions of the trajectory. The focus and goal of Phase 1 is to demonstrate the integration and performance of the propulsion system flowpath with the vehicle aerodynamics over the air-breathing trajectory. This demonstrator vehicle will have dual mode ramjetkcramjets, which include the inlet, combustor, and nozzle with geometrically scaled aerodynamic surface outer mold lines (OML) defining the forebody, boundary layer diverter, wings, and tail. The primary objective of this study is to demon- strate propulsion system performance and operability including the ram to scram transition, as well as to validate vehicle aerodynamics and propulsion airframe integration. To minimize overall risk and develop ment cost the effort will incorporate proven materials, use existing turbomachinery in the propellant delivery systems, launch from an existing unmanned remote launch facility, and use basic vehicle recovery techniques to minimize control and landing requirements. A second phase would demonstrate propulsion performance across all critical portions of a space launch trajectory (lift off through transition to all-rocket) integrated with flight-like vehicle systems.

14 CFR 121.387 - Flight engineer.

Science.gov (United States)

2010-01-01

... 14 Aeronautics and Space 3 2010-01-01 2010-01-01 false Flight engineer. 121.387 Section 121.387..., FLAG, AND SUPPLEMENTAL OPERATIONS Airman and Crewmember Requirements § 121.387 Flight engineer. No... holding a current flight engineer certificate. For each airplane type certificated after January 1, 1964...

The Next Generation Advanced Video Guidance Sensor: Flight Heritage and Current Development

Science.gov (United States)

Howard, Richard T.; Bryan, Thomas C.

2009-01-01

The Next Generation Advanced Video Guidance Sensor (NGAVGS) is the latest in a line of sensors that have flown four times in the last 10 years. The NGAVGS has been under development for the last two years as a long-range proximity operations and docking sensor for use in an Automated Rendezvous and Docking (AR&D) system. The first autonomous rendezvous and docking in the history of the U.S. Space Program was successfully accomplished by Orbital Express, using the Advanced Video Guidance Sensor (AVGS) as the primary docking sensor. That flight proved that the United States now has a mature and flight proven sensor technology for supporting Crew Exploration Vehicles (CEV) and Commercial Orbital Transport Systems (COTS) Automated Rendezvous and Docking (AR&D). NASA video sensors have worked well in the past: the AVGS used on the Demonstration of Autonomous Rendezvous Technology (DART) mission operated successfully in "spot mode" out to 2 km, and the first generation rendezvous and docking sensor, the Video Guidance Sensor (VGS), was developed and successfully flown on Space Shuttle flights in 1997 and 1998. This paper presents the flight heritage and results of the sensor technology, some hardware trades for the current sensor, and discusses the needs of future vehicles that may rendezvous and dock with the International Space Station (ISS) and other Constellation vehicles. It also discusses approaches for upgrading AVGS to address parts obsolescence, and concepts for minimizing the sensor footprint, weight, and power requirements. In addition, the testing of the various NGAVGS development units will be discussed along with the use of the NGAVGS as a proximity operations and docking sensor.

Nuptial flights behavior of the African weaver ant, Oecophylla longinoda Latreille (Hymenoptera: Formicidae) and weather factors triggering flights

DEFF Research Database (Denmark)

Nene, Wilson; Rwegasira, Gration; Nielsen, Mogens Gissel

2016-01-01

years, we found that sexuals aggregate on nest surfaces prior to flights. We also found that flights took place during the raining season, and all flights took place in evenings just before sunset. Further to these, days with flights were associated with higher relative humidity and less sun shine...... collection of mated queens to stock ant nurseries that supply ant colonies for IPM-programs....

An overview of integrated flight-propulsion controls flight research on the NASA F-15 research airplane

Science.gov (United States)

Burcham, Frank W., Jr.; Gatlin, Donald H.; Stewart, James F.

1995-01-01

The NASA Dryden Flight Research Center has been conducting integrated flight-propulsion control flight research using the NASA F-15 airplane for the past 12 years. The research began with the digital electronic engine control (DEEC) project, followed by the F100 Engine Model Derivative (EMD). HIDEC (Highly Integrated Digital Electronic Control) became the umbrella name for a series of experiments including: the Advanced Digital Engine Controls System (ADECS), a twin jet acoustics flight experiment, self-repairing flight control system (SRFCS), performance-seeking control (PSC), and propulsion controlled aircraft (PCA). The upcoming F-15 project is ACTIVE (Advanced Control Technology for Integrated Vehicles). This paper provides a brief summary of these activities and provides background for the PCA and PSC papers, and includes a bibliography of all papers and reports from the NASA F-15 project.

Theseus on Take-off for First Flight

Science.gov (United States)

1996-01-01

The Theseus prototype research aircraft takes off for its first test flight from NASA's Dryden Flight Research Center, Edwards, California, on May 24, 1996. The Theseus aircraft, built and operated by Aurora Flight Sciences Corporation, Manassas, Virginia, was a unique aircraft flown at NASA's Dryden Flight Research Center, Edwards, California, under a cooperative agreement between NASA and Aurora. Dryden hosted the Theseus program, providing hangar space and range safety for flight testing. Aurora Flight Sciences was responsible for the actual flight testing, vehicle flight safety, and operation of the aircraft. The Theseus remotely piloted aircraft flew its maiden flight on May 24, 1996, at Dryden. During its sixth flight on November 12, 1996, Theseus experienced an in-flight structural failure that resulted in the loss of the aircraft. As of the beginning of the year 2000, Aurora had not rebuilt the aircraft. Theseus was built for NASA under an innovative, $4.9 million fixed-price contract by Aurora Flight Sciences Corporation and its partners, West Virginia University, Morgantown, West Virginia, and Fairmont State College, Fairmont, West Virginia. The twin-engine, unpiloted vehicle had a 140-foot wingspan, and was constructed largely of composite materials. Powered by two 80-horsepower, turbocharged piston engines that drove twin 9-foot-diameter propellers, Theseus was designed to fly autonomously at high altitudes, with takeoff and landing under the active control of a ground-based pilot in a ground control station 'cockpit.' With the potential ability to carry 700 pounds of science instruments to altitudes above 60,000 feet for durations of greater than 24 hours, Theseus was intended to support research in areas such as stratospheric ozone depletion and the atmospheric effects of future high-speed civil transport aircraft engines. Instruments carried aboard Theseus also would be able to validate satellite-based global environmental change measurements. Dryden

A unified flight control methodology for a compound rotorcraft in fundamental and aerobatic maneuvering flight

Science.gov (United States)

Thorsen, Adam

This study investigates a novel approach to flight control for a compound rotorcraft in a variety of maneuvers ranging from fundamental to aerobatic in nature. Fundamental maneuvers are a class of maneuvers with design significance that are useful for testing and tuning flight control systems along with uncovering control law deficiencies. Aerobatic maneuvers are a class of aggressive and complex maneuvers with more operational significance. The process culminating in a unified approach to flight control includes various control allocation studies for redundant controls in trim and maneuvering flight, an efficient methodology to simulate non-piloted maneuvers with varying degrees of complexity, and the setup of an unconventional control inceptor configuration along with the use of a flight simulator to gather pilot feedback in order to improve the unified control architecture. A flight path generation algorithm was developed to calculate control inceptor commands required for a rotorcraft in aerobatic maneuvers. This generalized algorithm was tailored to generate flight paths through optimization methods in order to satisfy target terminal position coordinates or to minimize the total time of a particular maneuver. Six aerobatic maneuvers were developed drawing inspiration from air combat maneuvers of fighter jet aircraft: Pitch-Back Turn (PBT), Combat Ascent Turn (CAT), Combat Descent Turn (CDT), Weaving Pull-up (WPU), Combat Break Turn (CBT), and Zoom and Boom (ZAB). These aerobatic maneuvers were simulated at moderate to high advance ratios while fundamental maneuvers of the compound including level accelerations/decelerations, climbs, descents, and turns were investigated across the entire flight envelope to evaluate controller performance. The unified control system was developed to allow controls to seamlessly transition between manual and automatic allocations while ensuring that the axis of control for a particular inceptor remained constant with flight

14 CFR 415.115 - Flight safety.

Science.gov (United States)

2010-01-01

... 14 Aeronautics and Space 4 2010-01-01 2010-01-01 false Flight safety. 415.115 Section 415.115... TRANSPORTATION LICENSING LAUNCH LICENSE Safety Review and Approval for Launch of an Expendable Launch Vehicle From a Non-Federal Launch Site § 415.115 Flight safety. (a) Flight safety analysis. An applicant's...

Hingekeeled ajaloo kuumas tolmus / Jan Kaus

Index Scriptorium Estoniae

Kaus, Jan, 1971-

2011-01-01

Arvustus: Hargla, Indrek. Apteeker Melchior ja timuka tütar : kriminaalromaan vanast Tallinnast. Tallinn : Varrak, 2011 ja Aleksejev, Tiit. Kindel linn : lugu Esimesest ristisõjast. Tallinn : Varrak, 2011

Ilmusid Ollinovski ja Pessoa kogud

Index Scriptorium Estoniae

2009-01-01

Ollinovski, Jim. Aeroplaan esimesest pilgust. Tallinn : Pilgrim, 2009 ; Pessoa, Fernando. Tubakapood : ́Alvaro de Campose viimased luuletused. Tallinn : Pilgrim Group, 2009. Esitlus 2. dets. Tallinnas Von Krahli teatris

Kodakondsus - kas integratsiooni eeldus või tulemus? / Klara Hallik

Index Scriptorium Estoniae

Hallik, Klara

2000-01-01

Eestlaste ja mitteeestlaste ootused kodakondsuspoliitika suhtes on jätkuvalt vastandlikud. Ilm. ka: Integration of Estonian Society : monitoring 2000.- Tallinn, 2000 ; Integratsija Estonskogo obshtshestva : monitoring 2000.- Tallinn, 2000

[Musikwissenschaftliche Literatur] / Kristel Pappel

Index Scriptorium Estoniae

Pappel, Kristel, 1961-

1999-01-01

Tutvustus: Urve Lippus (toim.). Music history writing and national culture. Proceedings of a seminar : Tallinn, Detsember 1-3, 1995. Eesti muusikaloo toimetised 1. Tallinn : Eesti Keele Instituut, 1995

Tekst ja subjekt. Tartu koolkonna teine põlvkond / Marek Tamm

Index Scriptorium Estoniae

Tamm, Marek, 1973-

1997-01-01

Arvustus: Lotman, Mihhail. Mandelshtam i Pasternak : popõtka kontrastivnoi poetiki. Tallinn : Aleksandra, 1996. (Biblioteka zhurnala Tallinn); Torop, Peeter. Dostojevski : istorija i ideologija. Tartu : Tartu Ülikooli Kirjastus, 1997

Vaike Kiik-Salupere doktoritööst "Esinemiseks valmistumine ja esinemisärevusega toimetulek klassikaliste lauljate vokaalpedagoogikas" / Allan Vurma

Index Scriptorium Estoniae

Vurma, Allan, 1955-

2014-01-01

Arvustus: Kiik-Salupere, Vaike. Performance preparation and coping with performance anxiety in the vocal pedagogy of classical singers. Tallinn : Tallinn University, 2013. (Tallinna Ülikooli sotsiaalteaduste dissertatsioonid ; 64)

Kes on tõusmas relvile? / Jürgen Rooste

Index Scriptorium Estoniae

Rooste, Jürgen, 1979-

2004-01-01

Arvustus: Oja, Martin., keelatud raamat : tekste 1996-2000. Tallinn : 9 Koma, 2003 ; Klaus, Eduard. Pommikutsikas. Tartu : Ilmamaa, 2003 ; Mölter, Artur. Leitud hing... ja purunenud süda. Põltsamaa : A. Mölter, 2003 ; Kera, Mihkel. Tähelepanekuid noorusaastatest. I. k. : Kirja Kerrallaan, 2003 ; Valme, Villem. Artur Tõhu unenägu. Tallinn : Paala Järv, 2003 ; Valdmann, Astrid, Kagovere, Ott. Haiged lapsed. Sutlema (Raplamaa) : A. Valdmann, 2004 ; Olematu, Olev. Ederlezi. [Tallinn] : Huma, 2003

Retrieving Balloon Data in Flight

Data.gov (United States)

National Aeronautics and Space Administration — NASA's Ultra Long Duration Balloon (ULDB) program will soon make flights lasting up to 100 days. Some flights may generate high data rates and retrieving this data...

First PET scans in Estonia

International Nuclear Information System (INIS)

Nazarenko, Sergei

2003-01-01

First PET scans in Estonia were performed on 25th November 2002 in North Estonia Regional Hospital, Tallinn. Six patients with melanoma underwent scanning with FDG. This event was a result of thorough extensive preparations first started in 2000 during the European Association of Nuclear Medicine congress in Paris. During the congress first contacts were made with providers of mobile PET units. At the same time negotiations were begun with potential FDG suppliers. For the introduction of PET in Estonia mobile truckmounted scanning technology was chosen due to low level of initial investments. Of particular importance was also availability of maintenance personnel from the device providers. A significant prerequisite was potential availability of FDG from the neighbourhood - Finland and Sweden. The latter avoided the necessity for investments into local cyclotrons and local FDG production. For the first scanning experience the dedicated truckmounted PET-camera Accel, Siemens was brought by the International Hospital Group (IHG, Amersfoort, Netherlands). The device arrived by ferry from Stockholm to Tallinn harbour at 10 o'clock in the morning and left by ferry for Helsinki at 23 o'clock. The team-on-truck consisted of one technician for device operation, two drivers and two company representatives. North Estonia Regional Hospital provided three additional technicians for patient preparation and FDG injection, one nuclear medicine doctor and one specialist of biomedical engineering and medical physics. The FDG was provided by MAP Medical Technologies, Schering, Helsinki, Finland. The shipments were made by air. This was possible due to small distance between Tallinn and Helsinki of approximately 80 km due to the regular flight connections between the two cities. The FDG was shipped in two lots with a time interval of 4 hours. The patient selection was based on clinical and histopathology data. In all six patients the exam was justified for detailied staging and

14 CFR 417.107 - Flight safety.

Science.gov (United States)

2010-01-01

... 14 Aeronautics and Space 4 2010-01-01 2010-01-01 false Flight safety. 417.107 Section 417.107... TRANSPORTATION LICENSING LAUNCH SAFETY Launch Safety Responsibilities § 417.107 Flight safety. (a) Flight safety... safety system that satisfies subpart D of this part as follows, unless § 417.125 applies. (1) In the...

Improved model for solar cosmic ray exposure in manned Earth orbital flights

International Nuclear Information System (INIS)

Wilson, J.W.; Nealy, J.E.; Atwell, W.; Cucinotta, F.A.; Shinn, J.L.; Townsend, L.W.

1990-06-01

A calculational model is derived for use in estimating Solar cosmic ray exposure to critical body organs in low-Earth orbit at the center of a large spherical shield of fixed thickness. The effects of the Earth's geomagnetic field and the astronauts' self-shielding are evaluated explicitly. The geomagnetic field model is an approximate tilted eccentric dipole with geomagnetic storms represented as a uniform-impressed field. The storm field is related to the planetary geomagnetic index K(sub p). The code is applied to the Shuttle geometry using the Shuttle mass distribution surrounding two locations on the flight deck. The Shuttle is treated as pure aluminum and the astronaut as soft tissue. Short-term, average fluence over a single orbit is calculated as a function of the location of the lines of nodes or long-term averages over all lines of nodes for a fixed inclination

Mini-Sniffer II in Flight

Science.gov (United States)

1976-01-01

This photograph shows the second Mini-Sniffer undergoing flight testing over Rogers Dry Lake in Edwards, California. This version of the Mini-Sniffer lacked the canard of the original version and had wing tips and tail booms added. The Mini-Sniffer was a remotely controlled, propeller-driven vehicle developed at the NASA Flight Research Center (which became the Dryden Flight Research Center, Edwards, California, in 1976) as a potential platform to sample the upper atmosphere for pollution. The vehicle, flown from 1975 to 1977, was one of the earliest attempts by NASA to develop an aircraft that could sense turbulence and measure natural and human-produced atmospheric pollutants at altitudes above 80,000 feet with a variable-load propeller that was never flight-tested. Three Mini-Sniffer vehicles were built. The number 1 Mini-Sniffer vehicle had swept wings with a span of 18 feet and canards on the nose. It flew 12 flights with the gas-powered engine at low altitudes of around 2,500 feet. The number 1 vehicle was then modified into version number 2 by removing the canards and wing rudders and adding wing tips and tail booms. Twenty flights were made with this version, up to altitudes of 20,000 feet. The number 3 vehicle had a longer fuselage, was lighter in weight, and was powered by the non-air-breathing hydrazine engine designed by NASA's Johnson Space Center in Houston, Texas. This version was designed to fly a 25-pound payload to an altitude of 70,000 feet for one hour or to climb to 90,000 feet and glide back. The number 3 Mini-Sniffer made one flight to 20,000 feet and was not flown again because of a hydrazine leak problem. All three versions used a pusher propeller to free the nose area for an atmospheric-sampling payload. At various times the Mini-Sniffer has been considered for exploration in the carbon dioxide atmosphere of the planet Mars, where the gravity (38 percent of that on Earth) would reduce the horsepower needed for flight.

Young PHD's in Human Space Flight

Science.gov (United States)

Wilson, Eleanor

2002-01-01

The Cooperating Hampton Roads Organizations for Minorities in Engineering (CHROME) in cooperation with the NASA Office of Space Flight, Human Exploration and Development of Space Enterprise sponsored a summer institute, Young PHD#s (Persons Having Dreams) in Human Space Flight. This 3-day institute used the curriculum of a workshop designed for space professionals, 'Human Space Flight-Analysis and Design: An Integrated, Systematic Approach.' The content was tailored to a high school audience. This institute seeks to stimulate the interest of pre-college students in space flight and motivate them to pursue further experiences in this field. Additionally, this institute will serve as a pilot model for a pre- collegiate training program that can be replicated throughout the country. The institute was complemented with a trip to the Goddard Space Flight Center.

Vector magnetic fields in sunspots. I - Stokes profile analysis using the Marshall Space Flight Center magnetograph

Science.gov (United States)

Balasubramaniam, K. S.; West, E. A.

1991-01-01

The Marshall Space Flight Center (MSFC) vector magnetograph is a tunable filter magnetograph with a bandpass of 125 mA. Results are presented of the inversion of Stokes polarization profiles observed with the MSFC vector magnetograph centered on a sunspot to recover the vector magnetic field parameters and thermodynamic parameters of the spectral line forming region using the Fe I 5250.2 A spectral line using a nonlinear least-squares fitting technique. As a preliminary investigation, it is also shown that the recovered thermodynamic parameters could be better understood if the fitted parameters like Doppler width, opacity ratio, and damping constant were broken down into more basic quantities like temperature, microturbulent velocity, or density parameter.

Raamatuid / Juhan Habicht

Index Scriptorium Estoniae

Habicht, Juhan, 1954-

1992-01-01

Raamatud: Kareva, Doris. Kuuhobune. [Tallinn] : Katherine, [1992]. Imelik, Olaf. Tõde - kõige kaunim oled sa alasti. Tallinn : Mats, [1992]. Murutar, Kati. Naisena sündinud. [Pärnu] : Perona, 1992

B. B. ja järelpõlved / Ave Mattheus

Index Scriptorium Estoniae

Mattheus, Ave

2007-01-01

Arvustus: Enzensberger, Hans Magnus. Tõmba sobimatu maha / saksa keelest tlk. Maarja Kangro. Tallinn : Kultuurileht, 2006 (Loomingu Raamatukogu ; 33) ; Brecht, Bertolt. Luulet / koost. Märt Väljataga. Tallinn : Vagabund, 2007

Sündinud kunstnikuks - kahe Eestis kasvanud juudi lugu / Rein Veidemann

Index Scriptorium Estoniae

Veidemann, Rein, 1946-

2009-01-01

Arvustus: Tali, Piret. Eino Baskin. Naer läbi pisarate / kirja pannud Piret Tali. [Tallinn] : Fookus Meedia, [2009] ; Tammer, Enno. Simon Levin : sündinud advokaadiks. [Tallinn] : Tammerraamat, 2009

Raamatureisid Veneetsiasse / Margus Haav

Index Scriptorium Estoniae

Haav, Margus, 1969-

2005-01-01

Arvustus: Girardi, Robert. Vaporetto 13 / ingl. k. tlk. Karin Suursalu. Tallinn : Kultuurileht, 2005. (Loomingu Raamatukogu) ; Raittila, Hannu. Canal Grande : [romaan] / tõlkinud Aivo Lõhmus. Tallinn : Varrak, 2003 (Moodne aeg)

Sajandilõpu noori autoreid : Kruoganist Urduni / Piret Viires

Index Scriptorium Estoniae

Viires, Piret, 1963-

1999-01-01

Arvustus: Kruogan / koost. Hedda Maurer. Tallinn : Vares, 1998 ; Hea raamat / NAK ; toim. Indrek Särg. Tartu : Eesti Kostabi Selts, 1998 ; Harakkiri. Tallinn : Erakkond, 1999 ; Urdu : [kirjanduslik kogumik]. Rewal, 1999

Keskkond / Peep Pobbul

Index Scriptorium Estoniae

Pobbul, Peep

2004-01-01

Ilmunud ka: 2003 : annual report : [Eesti Raudtee]. - Tallinn, 2004, lk. 40-41; 2003 : godovoi ottshjot : [Eesti Raudtee]. - Tallinn, 2004, lk. 40-41. AS-i Eesti Raudtee keskkonna-alastest projektidest

Õhuloss kuristiku kohal / Raul Sulbi

Index Scriptorium Estoniae

Sulbi, Raul

2002-01-01

Arvustus: Pelevin, Viktor. Sinine latern / vene keelest tõlkinud Vladimir Indrikson. Tallinn : Atlantis, 2002 ; Pelevin, Viktor. Omon Ra ; Generation "P" / vene keelest tõlkinud Maiga Varik. Tallinn : Varrak, 2002

The response of an RC line MWPC to primary cosmic rays. [Multi-Wire Proportional Counter

Science.gov (United States)

Gregory, J. C.; Selig, W. J.; Austin, R. W.; Derrickson, J. H.; Parnell, T. A.

1978-01-01

A simple 50 x 50 sq cm MWPC plane was arranged as an RC-line and flown on a balloon flight with the MSFC-UAH Cosmic Ray experiment. Positions of primary cosmic ray tracks in the RC-line were determined by the risetime method and compared with the expected position as indicated by a best line fitted through four planes of the conventional MWPC hodoscope. Mean errors were estimated for sea-level muons, and CNO group and iron group particles. It is believed that the delta-rays accompanying the primaries degraded the position resolution. Measured standard deviations allowing for uncertainty in the true track position are of the order of 1 cm or less in the primary charge region between 7 and 26.

Lessons Learned and Flight Results from the F15 Intelligent Flight Control System Project

Science.gov (United States)

Bosworth, John

2006-01-01

A viewgraph presentation on the lessons learned and flight results from the F15 Intelligent Flight Control System (IFCS) project is shown. The topics include: 1) F-15 IFCS Project Goals; 2) Motivation; 3) IFCS Approach; 4) NASA F-15 #837 Aircraft Description; 5) Flight Envelope; 6) Limited Authority System; 7) NN Floating Limiter; 8) Flight Experiment; 9) Adaptation Goals; 10) Handling Qualities Performance Metric; 11) Project Phases; 12) Indirect Adaptive Control Architecture; 13) Indirect Adaptive Experience and Lessons Learned; 14) Gen II Direct Adaptive Control Architecture; 15) Current Status; 16) Effect of Canard Multiplier; 17) Simulated Canard Failure Stab Open Loop; 18) Canard Multiplier Effect Closed Loop Freq. Resp.; 19) Simulated Canard Failure Stab Open Loop with Adaptation; 20) Canard Multiplier Effect Closed Loop with Adaptation; 21) Gen 2 NN Wts from Simulation; 22) Direct Adaptive Experience and Lessons Learned; and 23) Conclusions

Pigeons (C. livia Follow Their Head during Turning Flight: Head Stabilization Underlies the Visual Control of Flight

Directory of Open Access Journals (Sweden)

Ivo G. Ros

2017-12-01

Full Text Available Similar flight control principles operate across insect and vertebrate fliers. These principles indicate that robust solutions have evolved to meet complex behavioral challenges. Following from studies of visual and cervical feedback control of flight in insects, we investigate the role of head stabilization in providing feedback cues for controlling turning flight in pigeons. Based on previous observations that the eyes of pigeons remain at relatively fixed orientations within the head during flight, we test potential sensory control inputs derived from head and body movements during 90° aerial turns. We observe that periods of angular head stabilization alternate with rapid head repositioning movements (head saccades, and confirm that control of head motion is decoupled from aerodynamic and inertial forces acting on the bird's continuously rotating body during turning flapping flight. Visual cues inferred from head saccades correlate with changes in flight trajectory; whereas the magnitude of neck bending predicts angular changes in body position. The control of head motion to stabilize a pigeon's gaze may therefore facilitate extraction of important motion cues, in addition to offering mechanisms for controlling body and wing movements. Strong similarities between the sensory flight control of birds and insects may also inspire novel designs of robust controllers for human-engineered autonomous aerial vehicles.

14 CFR 61.41 - Flight training received from flight instructors not certificated by the FAA.

Science.gov (United States)

2010-01-01

... the FAA. (a) A person may credit flight training toward the requirements of a pilot certificate or... flight instructor described in paragraph (a) of this section is only authorized to give endorsements to...

X-36 in Flight near Edge of Rogers Dry Lake during 5th Flight

Science.gov (United States)

1997-01-01

This photo shows the X-36 Tailless Fighter Agility Research Aircraft passing over the edge of Rogers Dry Lake as the remotely-piloted aircraft flies over Edwards Air Force Base on a June 1997 research flight. The NASA/Boeing X-36 Tailless Fighter Agility Research Aircraft program successfully demonstrated the tailless fighter design using advanced technologies to improve the maneuverability and survivability of possible future fighter aircraft. The program met or exceeded all project goals. For 31 flights during 1997 at the Dryden Flight Research Center, Edwards, California, the project team examined the aircraft's agility at low speed / high angles of attack and at high speed / low angles of attack. The aircraft's speed envelope reached up to 206 knots (234 mph). This aircraft was very stable and maneuverable. It handled very well. The X-36 vehicle was designed to fly without the traditional tail surfaces common on most aircraft. Instead, a canard forward of the wing was used as well as split ailerons and an advanced thrust-vectoring nozzle for directional control. The X-36 was unstable in both pitch and yaw axes, so an advanced, single-channel digital fly-by-wire control system (developed with some commercially available components) was put in place to stabilize the aircraft. Using a video camera mounted in the nose of the aircraft and an onboard microphone, the X-36 was remotely controlled by a pilot in a ground station virtual cockpit. A standard fighter-type head-up display (HUD) and a moving-map representation of the vehicle's position within the range in which it flew provided excellent situational awareness for the pilot. This pilot-in-the-loop approach eliminated the need for expensive and complex autonomous flight control systems and the risks associated with their inability to deal with unknown or unforeseen phenomena in flight. Fully fueled the X-36 prototype weighed approximately 1,250 pounds. It was 19 feet long and three feet high with a wingspan of

Post-Flight Data Analysis Tool

Science.gov (United States)

George, Marina

2018-01-01

A software tool that facilitates the retrieval and analysis of post-flight data. This allows our team and other teams to effectively and efficiently analyze and evaluate post-flight data in order to certify commercial providers.

14 CFR 61.193 - Flight instructor privileges.

Science.gov (United States)

2010-01-01

... than Flight Instructors With a Sport Pilot Rating § 61.193 Flight instructor privileges. A person who...; (e) An aircraft rating; (f) An instrument rating; (g) A flight review, operating privilege, or...

Melchior: Eesti tulevane ikoon / Jaan Martinson

Index Scriptorium Estoniae

Martinson, Jaan, 1960-

2010-01-01

Tutvustus: Hargla, Indrek, pseud. Apteeker Melchior ja Oleviste mõistatus : kriminaalromaan vanast Tallinnast. Tallinn : Varrak, 2010 ; Hargla, Indrek, pseud. Apteeker Melchior ja Rataskaevu viirastus : kriminaalromaan vanast Tallinnast. Tallinn : Varrak, 2010

Hingelised kriminaalid / Vaapo Vaher

Index Scriptorium Estoniae

Vaher, Vaapo, 1945-

1994-01-01

Raamatututvustus: Ränik, Valeria. Ajast väljas. Viljandi : Ajaleht "Sakala", 1994. Kallas, Aino. Pärjapunuja. Tallinn : Eesti Raamat, 1994. Wallace, Edgar. Kuldne iidol ; Kolme tamme saladus. Tallinn : Perioodika, 1994

Aegade varjud : [luuletused] / Karl Ast Rumor

Index Scriptorium Estoniae

Ast Rumor, Karl

2007-01-01

Sisu : Meie ja nemad ; Öisel teel ; Luikede laul ; Crescendo ; Needmine ; Bajazzo ; Kurbtus ; Minevikule ; Tunnistus ; Punased lilled. Varem ilmunud ""Edasi" jõulualbum 4". Tallinn 1911 ; "Meie Sõna 1". Tallinn 1911

Infotehnoloogiateenistus / Meelis Kukk

Index Scriptorium Estoniae

Kukk, Meelis

2004-01-01

Ilmunud ka: 2003 : annual report : [Eesti Raudtee]. - Tallinn, 2004, lk. 36; 2003 : godovoi ottshjot : [Eesti Raudtee]. - Tallinn, 2004, lk. 36. Ülevaade AS-i Eesti Raudtee infotehnoloogiteenistuse tegvusest 2003. aastal

Planeeringute uus veebiregister sai valmis

Index Scriptorium Estoniae

2015-01-01

Varasem register http://ehitus.tallinn.ee jääb projekteerimistingimuste ja ehitusprojektide jaoks, Tallinna uus planeeringute register http://tpr.tallinn.ee võimaldab kõigil huvitatutel linnaplaneerimises arvamust avaldada

Enclosure enhancement of flight performance

KAUST Repository

Ghommem, Mehdi; Garcia, Daniel; Calo, Victor M.

2014-01-01

We use a potential flow solver to investigate the aerodynamic aspects of flapping flights in enclosed spaces. The enclosure effects are simulated by the method of images. Our study complements previous aerodynamic analyses which considered only the near-ground flight. The present results show that flying in the proximity of an enclosure affects the aerodynamic performance of flapping wings in terms of lift and thrust generation and power consumption. It leads to higher flight efficiency and more than 5% increase of the generation of lift and thrust.

Enclosure enhancement of flight performance

KAUST Repository

Ghommem, Mehdi

2014-08-19

We use a potential flow solver to investigate the aerodynamic aspects of flapping flights in enclosed spaces. The enclosure effects are simulated by the method of images. Our study complements previous aerodynamic analyses which considered only the near-ground flight. The present results show that flying in the proximity of an enclosure affects the aerodynamic performance of flapping wings in terms of lift and thrust generation and power consumption. It leads to higher flight efficiency and more than 5% increase of the generation of lift and thrust.

Data Mining of NASA Boeing 737 Flight Data: Frequency Analysis of In-Flight Recorded Data

Science.gov (United States)

Butterfield, Ansel J.

2001-01-01

Data recorded during flights of the NASA Trailblazer Boeing 737 have been analyzed to ascertain the presence of aircraft structural responses from various excitations such as the engine, aerodynamic effects, wind gusts, and control system operations. The NASA Trailblazer Boeing 737 was chosen as a focus of the study because of a large quantity of its flight data records. The goal of this study was to determine if any aircraft structural characteristics could be identified from flight data collected for measuring non-structural phenomena. A number of such data were examined for spatial and frequency correlation as a means of discovering hidden knowledge of the dynamic behavior of the aircraft. Data recorded from on-board dynamic sensors over a range of flight conditions showed consistently appearing frequencies. Those frequencies were attributed to aircraft structural vibrations.

Development and Flight Evaluation of an Emergency Digital Flight Control System Using Only Engine Thrust on an F-15 Airplane

Science.gov (United States)

Burcham, Frank W., Jr.; Maine, Trindel A.; Fullerton, C. Gordon; Webb, Lannie Dean

1996-01-01

A propulsion-controlled aircraft (PCA) system for emergency flight control of aircraft with no flight controls was developed and flight tested on an F-15 aircraft at the NASA Dryden Flight Research Center. The airplane has been flown in a throttles-only manual mode and with an augmented system called PCA in which pilot thumbwheel commands and aircraft feedback parameters were used to drive the throttles. Results from a 36-flight evaluation showed that the PCA system can be used to safety land an airplane that has suffered a major flight control system failure. The PCA system was used to recover from a severe upset condition, descend, and land. Guest pilots have also evaluated the PCA system. This paper describes the principles of throttles-only flight control; a history of loss-of-control accidents; a description of the F-15 aircraft; the PCA system operation, simulation, and flight testing; and the pilot comments.

Theseus Waits on Lakebed for First Flight

Science.gov (United States)

1996-01-01

The Theseus prototype remotely-piloted aircraft (RPA) waits on the lakebed before its first test flight from NASA's Dryden Flight Research Center, Edwards, California, on May 24, 1996. The Theseus aircraft, built and operated by Aurora Flight Sciences Corporation, Manassas, Virginia, was a unique aircraft flown at NASA's Dryden Flight Research Center, Edwards, California, under a cooperative agreement between NASA and Aurora. Dryden hosted the Theseus program, providing hangar space and range safety for flight testing. Aurora Flight Sciences was responsible for the actual flight testing, vehicle flight safety, and operation of the aircraft. The Theseus remotely piloted aircraft flew its maiden flight on May 24, 1996, at Dryden. During its sixth flight on November 12, 1996, Theseus experienced an in-flight structural failure that resulted in the loss of the aircraft. As of the beginning of the year 2000, Aurora had not rebuilt the aircraft. Theseus was built for NASA under an innovative, $4.9 million fixed-price contract by Aurora Flight Sciences Corporation and its partners, West Virginia University, Morgantown, West Virginia, and Fairmont State College, Fairmont, West Virginia. The twin-engine, unpiloted vehicle had a 140-foot wingspan, and was constructed largely of composite materials. Powered by two 80-horsepower, turbocharged piston engines that drove twin 9-foot-diameter propellers, Theseus was designed to fly autonomously at high altitudes, with takeoff and landing under the active control of a ground-based pilot in a ground control station 'cockpit.' With the potential ability to carry 700 pounds of science instruments to altitudes above 60,000 feet for durations of greater than 24 hours, Theseus was intended to support research in areas such as stratospheric ozone depletion and the atmospheric effects of future high-speed civil transport aircraft engines. Instruments carried aboard Theseus also would be able to validate satellite-based global environmental

Integrating Space Flight Resource Management Skills into Technical Lessons for International Space Station Flight Controller Training

Science.gov (United States)

Baldwin, Evelyn

2008-01-01

The Johnson Space Center s (JSC) International Space Station (ISS) Space Flight Resource Management (SFRM) training program is designed to teach the team skills required to be an effective flight controller. It was adapted from the SFRM training given to Shuttle flight controllers to fit the needs of a "24 hours a day/365 days a year" flight controller. More recently, the length reduction of technical training flows for ISS flight controllers impacted the number of opportunities for fully integrated team scenario based training, where most SFRM training occurred. Thus, the ISS SFRM training program is evolving yet again, using a new approach of teaching and evaluating SFRM alongside of technical materials. Because there are very few models in other industries that have successfully tied team and technical skills together, challenges are arising. Despite this, the Mission Operations Directorate of NASA s JSC is committed to implementing this integrated training approach because of the anticipated benefits.

F-14 in banked flight

Science.gov (United States)

1979-01-01

NASA 991, an F-14 Navy Tomcat designated the F-14 (1X), is seen here in banked flight over the desert on a research flight at NASA's Dryden Flight Research Center, Edwards, California. The F-14 was used at Dryden between 1979 and 1985 in extensive high-angle-of-attack and spin-control-and-recovery tests. The NASA/Navy program, which included 212 total flights, acheived considerable improvement in the F-14 high-angle-of-attack flying qualities, improved departure and spin resistance, and contributed to substantial improvements in reducing 'wing rock,' (i.e., tilting from one side to another), at high angles of attack. The Navy had been experiencing inadvertant spin entries caused by the F-14's aileron rudder interconnect. The NASA/Navy/Grumman team developed and tested 4 different configurations of the aileron rudder interconnect to address the spin problem. These problems prompted the Navy to ask the manufacturer, Grumman, and NASA to investigate the issue. NASA 991 had numerous special additions for high-angle-of-attack and spin-recovery research. These included a battery-powered auxiliary power unit, a flight test nose boom, and a special spin recovery system, consisting of forward mounted, hydraulically actuated canards and an emergency spin chute. NASA's F-14 was first flown by NASA research pilots, but was later flown by Grumman, and by Navy test pilots from Patuxent River Naval Air Station (NAS). The Navy test flights with the spin research vehicle constituted the first program that incorporated air combat maneuvering in its test flights at Dryden. The Navy brought F-14s from Point Mugu and Miramar NAS in San Diego to test the new spin control laws in combat situations. Although the new control laws proved valuable, the Navy did not incorporate them into production F-14s until the F-14D, nearly 15 years later.

An electrostatic beam line for accelerator mass spectroscopy of exotic particles

International Nuclear Information System (INIS)

Elmore, D.; Kubik, P.W.; Hemmick, T.; Teng, R.; Kagan, H.; Haas, P.; Boyd, R.N.; Turner, R.; Nitz, D.; Ciampa, D.; Olsen, S.L.; Gentile, T.; Haelen, T.

1985-01-01

An all-electrostatic charged particle spectrometer has been constructed to perform high sensitivity searches for exotic states of matter. This spectrometer consists of an electrosatic beam line capable of mass independent charged particle transport and selection together with time-of-flight, energy loss and total energy detectors. This system has been used in conjunction with the tandem electrostatic accelerator at the Nuclear Structure Research Laboratory of the University of Rochester to search for fractionally charged or anomalously heavy particles. (orig.)

Majaraamatud - ühtne tervik ja väärikalt hoitud detailid / Yoko Alender

Index Scriptorium Estoniae

Alender, Yoko, 1979-

2011-01-01

Tutvustus: Tallinna maja : hoonetüübi areng ja säästev uuendamine / koostanud Mark Sepp ja Tallinna Kultuuriväärtuste Amet. Tallinn, 2010; Lenderi maja : hoonetüübi areng ja säästev uuendamine / koostanud Anni Martin ja Tallinna Kultuuriväärtuste Amet. Tallinn, 2009; Funktsionalistlik maja : eramu ja väike kortermaja / koostanud Monika Eensalu ja Tallinna Kultuuriväärtuste Amet. Tallinn, 2011. Vanade majade säilitamisest

Tõlkimise teooriast ja praktikast / Märt Väljataga

Index Scriptorium Estoniae

Väljataga, Märt, 1965-

2008-01-01

Tõlkimisest ja tõlkekriitikast. 2008. a. ilmunud tõlkimist käsitlevatest väljaannetest: Lange, Anne. Tõlkimise aabits. Tallinn : Valgus, 2008 ; Saluäär, Anu. Põhjamaadest ja Eestist. Tallinn : Eesti Keele Sihtasutus, 2008 ; Kaldjärv, Klaarika. Autor, jutustaja, tõlkija : Borgese autofiktsioonid eesti keeles. Tartu : Tartu Ülikooli Kirjastus, 2008 ; Ain Kaalep 80 : konverentsikogumik. Tartu : Eesti Kirjanduse Selts, 2008. (Eesti Kirjanduse Seltsi aastaraamat 2006 ; 32) ; Steiner, George. Valik esseid / tlk. Triinu Pakk. Tallinn : Kultuurileht, 2008

Design and analysis of advanced flight planning concepts

Science.gov (United States)

Sorensen, John A.

1987-01-01

The objectives of this continuing effort are to develop and evaluate new algorithms and advanced concepts for flight management and flight planning. This includes the minimization of fuel or direct operating costs, the integration of the airborne flight management and ground-based flight planning processes, and the enhancement of future traffic management systems design. Flight management (FMS) concepts are for on-board profile computation and steering of transport aircraft in the vertical plane between a city pair and along a given horizontal path. Flight planning (FPS) concepts are for the pre-flight ground based computation of the three-dimensional reference trajectory that connects the city pair and specifies the horizontal path, fuel load, and weather profiles for initializing the FMS. As part of these objectives, a new computer program called EFPLAN has been developed and utilized to study advanced flight planning concepts. EFPLAN represents an experimental version of an FPS. It has been developed to generate reference flight plans compatible as input to an FMS and to provide various options for flight planning research. This report describes EFPLAN and the associated research conducted in its development.

[Paulo Coelho. Zahir ; Jan Kaus. Tema] / Aarne Biin

Index Scriptorium Estoniae

Biin, Aarne

2007-01-01

Tutvustus: Coelho, Paulo. Zahir : [romaan] / portugali keelest tõlkinud Anneli Tuulik, [Konstantinos Kavafise luuletuse uuskreeka keelest tõlkinud Mati Sirkel. Tallinn] : Pilgrim Group, 2005 ; Kaus, Jan. Tema : [romaan]. Tallinn : Tuum, 2006

Kasulikud raamatud lastega reisijatele / Lydia Aspen

Index Scriptorium Estoniae

Aspen, Lydia

2009-01-01

Tutvustus: London : laste reisijuht : suurlinna seiklused, mõistatused ja mängud. Tallinn : TEA Kirjastus, 2009 ; Pariis : laste reisijuht : suurlinna seiklused, mõistatused ja mängud. Tallinn : TEA Kirjastus, 2009

Kolm plaati eesti klassikast : Cyrillus Kreegi "Requiemi" kaks ettekanet ja "Eesti heliloojad V" / Kerri Kotta

Index Scriptorium Estoniae

Kotta, Kerri, 1969-

2009-01-01

Arvustus : Kreek, Cyrillus. Requiem. Musica sacra. Tampere : Alba, 2007. Kreek, Cyrillus. Requiem. Tõnu Kõrvits. Kreegi vihik. [Tallinn] : Eesti Filharmoonia Kammerkoor, 2008. Eesti heliloojad V. Tallinn : Eesti Rahvusringhääling, 2008

Simulation model for the Boeing 720B aircraft-flight control system in continuous flight.

Science.gov (United States)

1971-08-01

A mathematical model of the Boeing 720B aircraft and autopilot has been derived. The model is representative of the 720B aircraft for continuous flight within a flight envelope defined by a Mach number of .4 at 20,000 feet altitude in a cruise config...

Flight Test Results for the F-16XL With a Digital Flight Control System

Science.gov (United States)

Stachowiak, Susan J.; Bosworth, John T.

2004-01-01

In the early 1980s, two F-16 airplanes were modified to extend the fuselage length and incorporate a large area delta wing planform. These two airplanes, designated the F-16XL, were designed by the General Dynamics Corporation (now Lockheed Martin Tactical Aircraft Systems) (Fort Worth, Texas) and were prototypes for a derivative fighter evaluation program conducted by the United States Air Force. Although the concept was never put into production, the F-16XL prototypes provided a unique planform for testing concepts in support of future high-speed supersonic transport aircraft. To extend the capabilities of this testbed vehicle the F-16XL ship 1 aircraft was upgraded with a digital flight control system. The added flexibility of a digital flight control system increases the versatility of this airplane as a testbed for aerodynamic research and investigation of advanced technologies. This report presents the handling qualities flight test results covering the envelope expansion of the F-16XL with the digital flight control system.

Reactions of Air Transport Flight Crews to Displays of Weather During Simulated Flight