Pressure Based Reference System For Aircraft Attitude Measurement

Kód výsledku v 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>

Výsledek na webu

<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>

Jazyk výsledku

angličtina

Název v původním jazyce

Pressure Based Reference System For Aircraft Attitude Measurement

Popis výsledku v původním jazyce

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

Název v anglickém jazyce

Pressure Based Reference System For Aircraft Attitude Measurement

Popis výsledku anglicky

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

Druh

D - Stať ve sborníku

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

—

Projekt

<a href="/cs/project/TA01030651" target="_blank" >TA01030651: Využití asistivních technologií pro zvýšení bezpečnosti letu letadel, létajícího personálu a pozemních účastníků leteckého provozu v normálním provozu a při výskytu mimořádných situací</a><br>

Návaznosti

S - Specificky vyzkum na vysokych skolach

Rok uplatnění

2013

Kód důvěrnosti údajů

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

Název statě ve sborníku

DASC 2013 - 32nd Digital Avionics Systems Conference 2013

ISBN

978-1-4799-1538-5

ISSN

2155-7195

e-ISSN

—

Počet stran výsledku

12

Strana od-do

"4C41"-"4C414"

Název nakladatele

AIAA

Místo vydání

Reston, VA

Místo konání akce

Syracuse

Datum konání akce

6. 10. 2013

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

000350222201033