DocumentCode :
1733489
Title :
A filtering method of gyroscope random drift for Miniature Unmanned Helicopter
Author :
Pan, Vue ; Song, Ping ; Li, KeJie ; Lin, Ran ; Huang, Wei
Author_Institution :
Sch. of Mechatronical Eng., Beijing Inst. of Technol., Beijing, China
Volume :
2
fYear :
2011
Firstpage :
730
Lastpage :
734
Abstract :
Low-cost MEMS gyroscopes used in the Miniature Unmanned Helicopter (MUH) have great random drift. In order to improve the performance of MEMS gyroscopes, a one-order AR model was established for the random drift. Then Sage-Husa adaptive Kalman filter was applied to process the random drift signal. Experiments were carried out to verify the validity of the method. Tests results demonstrate that the method based on AR model and Sage-Husa adaptive Kalman filter is convenient and effective and it significantly reduces random drift. Compared to conventional Kalman filter, Sage-Husa adaptive Kalman filter can estimate statistic characteristics of system noise and measurement noise and modify filter parameters on-time. It improves stability and adaptability and thus can give a more accurate filtering result.
Keywords :
Kalman filters; autonomous aerial vehicles; gyroscopes; micromechanical devices; Sage-Husa adaptive Kalman filter; filtering method; gyroscope random drift; low-cost MEMS gyroscopes; measurement noise; miniature unmanned helicopter; one-order AR model; random drift signal; system noise; Adaptation models; Equations; Gyroscopes; Kalman filters; Lead; Mathematical model; Size measurement; AR model; MUH; Sage-Husa adaptive Kalman filter; gyroscope random drift;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Science and Network Technology (ICCSNT), 2011 International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4577-1586-0
Type :
conf
DOI :
10.1109/ICCSNT.2011.6182068
Filename :
6182068
Link To Document :
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