Modular Navigation System for Unmanned Aerial Vehicles

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F13%3A00205548" target="_blank" >RIV/68407700:21230/13:00205548 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Modular Navigation System for Unmanned Aerial Vehicles
Original language description
This paper describes a modular navigation system for precise attitude (pitch, roll, and yaw angles) and position determination. The system consists of an inertial measurement unit, GPS receiver, magnetometer, electrolytic tilt sensors, and pressure sensors. Raw data from all sensors were compensated for deterministic errors, pre-processed, and used for attitude and position determination, which was done onboard an unmanned aerial vehicle. The data were also stored for post-processing. In both real-timeand offline methods the evaluation of navigation performance was based on Kalman filtering algorithms. The navigation system was tested using the UAV Bellanca Super Decathlon XXL. The accuracy of the evaluation as well as the performance was evaluated with respect to a precise multi-antenna GPS system.
Czech name
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Czech description
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Publication year
2013
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
ICMT'13 - Proceedings of the International Conference on Military Technologies
ISBN
978-80-7231-917-6
ISSN
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e-ISSN
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Number of pages
10
Pages from-to
1-10
Publisher name
Univerzita obrany
Place of publication
Brno
Event location
Brno
Event date
May 22, 2013
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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