Aerometric system for general aviation

Result code in 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>
Result on the web
<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>

Result language
angličtina
Original language name
Aerometric system for general aviation
Original language description
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.
Czech name
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Czech description
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Publication year
2015
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
2015 International Conference on Military Technologies (ICMT)
ISBN
978-80-7231-976-3
ISSN
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e-ISSN
—
Number of pages
6
Pages from-to
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Publisher name
IEEE Czechoslovakia Section
Place of publication
Praha
Event location
Brno
Event date
May 19, 2015
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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