Development of Navigation System for Unmanned Vehicles and Ultra-light Aircrafts

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F15%3A00229836" target="_blank" >RIV/68407700:21230/15:00229836 - isvavai.cz</a>

Výsledek na webu

<a href="http://radio.feld.cvut.cz/conf/poster2015/" target="_blank" >http://radio.feld.cvut.cz/conf/poster2015/</a>

DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Development of Navigation System for Unmanned Vehicles and Ultra-light Aircrafts

Popis výsledku v původním jazyce

Nowadays, the navigation systems play a key role in wide range of civil and military applications. Their performance and accuracy depend on used sensors. The most precise and also most expensive sensors are ring laser gyroscopes and servo accelerometerswhich usage is limited by their price. A cheaper alternative can be MEMS based sensors. Despite the MEMS inertial sensors have a lot advantages, they have also some weaknesses such as low resolution, noisy output, worse bias stability, etc. For these reasons they are not able to provide a navigation solution and thus the adding sources take place. This paper describes the hardware realization of navigation system for unmanned aerial vehicles and small aircrafts. The navigation system consists of tri-axial FXOS8700 accelerometer combined with tri-axial magnetometer and triad of ADXRS453 gyroscopes. This system is aided by absolute pressure sensor HSCMAND015PA2A3 for vertical corrections and by GPS receiver MAX-M8 to correct the position

Název v anglickém jazyce

Development of Navigation System for Unmanned Vehicles and Ultra-light Aircrafts

Popis výsledku anglicky

Nowadays, the navigation systems play a key role in wide range of civil and military applications. Their performance and accuracy depend on used sensors. The most precise and also most expensive sensors are ring laser gyroscopes and servo accelerometerswhich usage is limited by their price. A cheaper alternative can be MEMS based sensors. Despite the MEMS inertial sensors have a lot advantages, they have also some weaknesses such as low resolution, noisy output, worse bias stability, etc. For these reasons they are not able to provide a navigation solution and thus the adding sources take place. This paper describes the hardware realization of navigation system for unmanned aerial vehicles and small aircrafts. The navigation system consists of tri-axial FXOS8700 accelerometer combined with tri-axial magnetometer and triad of ADXRS453 gyroscopes. This system is aided by absolute pressure sensor HSCMAND015PA2A3 for vertical corrections and by GPS receiver MAX-M8 to correct the position

Druh

D - Stať ve sborníku

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

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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

Proceedings of the 19th International Scientific Student Conferenece POSTER 2015

ISBN

978-80-01-05499-4

ISSN

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e-ISSN

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Počet stran výsledku

5

Strana od-do

1-5

Název nakladatele

Czech Technical University in Prague

Místo vydání

Praha

Místo konání akce

Praha

Datum konání akce

14. 5. 2015

Typ akce podle státní příslušnosti

EUR - Evropská akce

Kód UT WoS článku

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