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
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;
Conference_Titel :
Intelligent Control and Automation (WCICA), 2012 10th World Congress on
Conference_Location :
Beijing
Print_ISBN :
978-1-4673-1397-1
DOI :
10.1109/WCICA.2012.6358106