Pressure Based Reference System For Aircraft Attitude Measurement
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F13%3A00208414" target="_blank" >RIV/68407700:21230/13:00208414 - isvavai.cz</a>
Result on the web
<a href="http://dx.doi.org/10.1109/DASC.2013.6712588" target="_blank" >http://dx.doi.org/10.1109/DASC.2013.6712588</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/DASC.2013.6712588" target="_blank" >10.1109/DASC.2013.6712588</a>
Alternative languages
Result language
angličtina
Original language name
Pressure Based Reference System For Aircraft Attitude Measurement
Original language description
This paper proposes a new system for aircraft attitude measurements. This measurement system can provide attitude reference measurements, in the other words Euler angles: pitch and roll angles, by a set of modified AHRS units and is aimed for ultra-lightcategory of aircrafts. The principle uses measurement of differential pressure between atmospheric static pressure and reference pressure. The static pressure is measured at tips of aircraft wings by differential pressure sensors with regards to the reference volume. Theory describing behavior of the gas in the closed reference volume is described in the first part of the paper. Two different arrangements of the pressure reference system are described with their advantages and disadvantages. These twoarrangements are modeled in Matlab Simulink and various ambient and inner influences are discussed in this part of the paper. Realization of different measurement system arrangements are presented in the next part of this paper. Parameter
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
<a href="/en/project/TA01030651" target="_blank" >TA01030651: Safety Improvement of Flight, Crew and Other Participants of Flight Transport in Normal and Emergency Situations by Assistive Technologies</a><br>
Continuities
S - Specificky vyzkum na vysokych skolach
Others
Publication year
2013
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
DASC 2013 - 32nd Digital Avionics Systems Conference 2013
ISBN
978-1-4799-1538-5
ISSN
2155-7195
e-ISSN
—
Number of pages
12
Pages from-to
"4C41"-"4C414"
Publisher name
AIAA
Place of publication
Reston, VA
Event location
Syracuse
Event date
Oct 6, 2013
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
000350222201033