DocumentCode
577688
Title
UKF based robust attitude control for helicopter
Author
Song, Qi ; Han, J.D. ; Jiang, Zhe
Author_Institution
State Key Lab. of Robot., Shenyang Inst. of Autom., Shenyang, China
fYear
2012
fDate
6-8 July 2012
Firstpage
1442
Lastpage
1446
Abstract
In order to handle the model uncertainty and the external disturbance, a robust attitude control method for helicopter robots is proposed in this paper. Unscented Kalman Filter (UKF) and backstepping technique are adopted in the attitude control design. Model-based backstepping control is presented to keep the desired helicopter attitude. UKF is employed for online estimation of both motion states and model errors of the helicopter. Such estimation results are further incorporated into the controller of helicopter. The backstepping control enhanced by real time model errors feedback can achieve a robust tracking performance even with the occurrence of external disturbance. Simulations conducted on the helicopter illustrate the effectiveness of the proposed attitude control.
Keywords
Kalman filters; attitude control; autonomous aerial vehicles; helicopters; mobile robots; robust control; telerobotics; UKF based robust attitude control; Unscented Kalman Filter; attitude control design; backstepping control; backstepping technique; external disturbance; helicopter robots; robust tracking performance; Adaptation models; Aerodynamics; Attitude control; Backstepping; Estimation; Helicopters; Uncertainty; UKF; attitude control; backstepping control; helicopter;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Automation (WCICA), 2012 10th World Congress on
Conference_Location
Beijing
Print_ISBN
978-1-4673-1397-1
Type
conf
DOI
10.1109/WCICA.2012.6358106
Filename
6358106
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