Aerometric system for general aviation

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F15%3A00233955" target="_blank" >RIV/68407700:21230/15:00233955 - isvavai.cz</a>

Výsledek na webu

<a href="http://dx.doi.org/10.1109/MILTECHS.2015.7153718" target="_blank" >http://dx.doi.org/10.1109/MILTECHS.2015.7153718</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1109/MILTECHS.2015.7153718" target="_blank" >10.1109/MILTECHS.2015.7153718</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Aerometric system for general aviation

Popis výsledku v původním jazyce

This article deals with design and partial realization of experimental aerometric system for general aviation. The height is determined by the barometric principle. However, the primary measurement of the pressure is performed by differential pressure sensor which is added by a low-cost absolute pressure sensor. This system allows a measurement of height, vertical speed and temperature of the environment. The accuracy of the system fulfills demands of civil aviation standards at low-cost. The article describes principle and advantages of height measurement by a differential pressure sensor, a design of an aerometric system and its components, and achieved measurement results. The article also outlines a possible future utilization of the system in thesector of ultralight planes and modern gliders.

Název v anglickém jazyce

Aerometric system for general aviation

Popis výsledku anglicky

This article deals with design and partial realization of experimental aerometric system for general aviation. The height is determined by the barometric principle. However, the primary measurement of the pressure is performed by differential pressure sensor which is added by a low-cost absolute pressure sensor. This system allows a measurement of height, vertical speed and temperature of the environment. The accuracy of the system fulfills demands of civil aviation standards at low-cost. The article describes principle and advantages of height measurement by a differential pressure sensor, a design of an aerometric system and its components, and achieved measurement results. The article also outlines a possible future utilization of the system in thesector of ultralight planes and modern gliders.

Druh

D - Stať ve sborníku

CEP obor

JA - Elektronika a optoelektronika, elektrotechnika

OECD FORD obor

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Projekt

—

Návaznosti

S - Specificky vyzkum na vysokych skolach

Rok uplatnění

2015

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

2015 International Conference on Military Technologies (ICMT)

ISBN

978-80-7231-976-3

ISSN

—

e-ISSN

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Počet stran výsledku

6

Strana od-do

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Název nakladatele

IEEE Czechoslovakia Section

Místo vydání

Praha

Místo konání akce

Brno

Datum konání akce

19. 5. 2015

Typ akce podle státní příslušnosti

EUR - Evropská akce

Kód UT WoS článku

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