DocumentCode
2121718
Title
A height controller design for miniature UAVs based on GPS and barometer
Author
Wang, Song ; Li, Juan ; Wang, Sihong
Author_Institution
UAV Res. Inst., Beihang Univ., Beijing, China
fYear
2012
fDate
21-23 April 2012
Firstpage
31
Lastpage
34
Abstract
With the limitations of airborne sensors configuration of conventional miniature UAVs, this paper proposes a practical real-time algorithm which can integrate barometric height and GPS altitude. This algorithm uses the GPS altitude to calibrate baro-altimeter on-line, without considering the motion model and maneuverability of carrier. Tests showed that the fusion algorithm has significantly improved measurement results of altitude information, combining short-term and dynamic performance of barometric height with long-term stability of GPS altitude. On this basis, the height controller was designed for miniature UAVs, and successfully applied to the flight control system of a small unmanned aerial vehicle for polar research, with the control error less than 10m during cruise stage.
Keywords
Global Positioning System; aircraft control; autonomous aerial vehicles; barometers; stability; GPS altitude stability; baro-altimeter online calibration; barometric height; flight control system; height controller design; miniature UAV; polar research; real-time algorithm; unmanned aerial vehicle; Aerospace control; Atmospheric measurements; Atmospheric modeling; Global Positioning System; Heuristic algorithms; Mercury (metals); Unmanned aerial vehicles; GPS; barometric; data fusion; hight control; miniature UAVs;
fLanguage
English
Publisher
ieee
Conference_Titel
Consumer Electronics, Communications and Networks (CECNet), 2012 2nd International Conference on
Conference_Location
Yichang
Print_ISBN
978-1-4577-1414-6
Type
conf
DOI
10.1109/CECNet.2012.6201800
Filename
6201800
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