Advanced Display and Position Angles Measurement Systems

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F12%3A00195272" target="_blank" >RIV/68407700:21230/12:00195272 - isvavai.cz</a>

Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Advanced Display and Position Angles Measurement Systems

Popis výsledku v původním jazyce

In this article we introduce a patented and a completely new concept of airplane orientation angles measurement system which is furthermore referred as a pressure reference system. The authors also propose an arrangement of a magnetometer unit with multiple sensors that perform online calibration of hard iron and soft iron distortions. These systems are mutually connected to a WiFi network with other modules, head-down and head-up displays. There is also description of common avionics system units and sensors and their relation to the new proposed system. General aviation accounts for about 77 percent of the total flight hours while the rest are routinely scheduled flights. General aviation operations range from short-distance flights in single engine light aircraft to long-distance international flights in private jets, aero-medical operations and flying for fun. Electronics onboard of the airplane nowadays costs around one third of the airplane total price which vary with the precision and capabilities of the electronics system. Demand for the more precise but low-cost navigation which could improve some safety issues is being solved by data fusion of different sets of low-cost micro-mechanical sensors. Mainly signals provided by global position system and triads of inertial measurement sensors are being investigated and tightly coupled. This combination is capable to provide position of the airplane and its orientation angles. This article presents a new system that provides new information about orientation angles which can be used within data fusion algorithms to increase precision of the displayed information.

Název v anglickém jazyce

Advanced Display and Position Angles Measurement Systems

Popis výsledku anglicky

In this article we introduce a patented and a completely new concept of airplane orientation angles measurement system which is furthermore referred as a pressure reference system. The authors also propose an arrangement of a magnetometer unit with multiple sensors that perform online calibration of hard iron and soft iron distortions. These systems are mutually connected to a WiFi network with other modules, head-down and head-up displays. There is also description of common avionics system units and sensors and their relation to the new proposed system. General aviation accounts for about 77 percent of the total flight hours while the rest are routinely scheduled flights. General aviation operations range from short-distance flights in single engine light aircraft to long-distance international flights in private jets, aero-medical operations and flying for fun. Electronics onboard of the airplane nowadays costs around one third of the airplane total price which vary with the precision and capabilities of the electronics system. Demand for the more precise but low-cost navigation which could improve some safety issues is being solved by data fusion of different sets of low-cost micro-mechanical sensors. Mainly signals provided by global position system and triads of inertial measurement sensors are being investigated and tightly coupled. This combination is capable to provide position of the airplane and its orientation angles. This article presents a new system that provides new information about orientation angles which can be used within data fusion algorithms to increase precision of the displayed information.

Druh

D - Stať ve sborníku

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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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

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2012

Kód důvěrnosti údajů

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

Název statě ve sborníku

ICAS 2012 - 28th Congress of the International Council of the Aeronautical Sciences - Proceedings

ISBN

978-1-62276-754-0

ISSN

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e-ISSN

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Počet stran výsledku

14

Strana od-do

3875-3888

Název nakladatele

ICAS - the International Council of the Aeronautical Science

Místo vydání

Brisbane

Místo konání akce

Brisbane

Datum konání akce

23. 9. 2012

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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