DocumentCode
2251266
Title
Sliding mode control attitude tracking of rigid spacecraft using adaptive back-stepping method
Author
Chunmei, Yu ; Kunfeng, Lu ; Yuanqing, Xia ; Hailiang, Liu
Author_Institution
Aerospace and Materials Engineering, National University of Defense Technology, Changsha 410073, China
fYear
2015
fDate
28-30 July 2015
Firstpage
3281
Lastpage
3286
Abstract
The attitude tracking control problem for a rigid spacecraft system is investigated in this paper. A novel adaptive approach is proposed with the utilization of sliding mode control (SMC) and backstepping technique (BT) to achieve accurate attitude tracking control for spacecraft system in the presence of inertia uncertainties and external disturbances. Finally, simulation results are presented to illustrate effectiveness of the control strategies.
Keywords
Adaptation models; Angular velocity; Attitude control; Backstepping; Quaternions; Space vehicles; Uncertainty; Adaptive control; Attitude tracking; Backstepping technique; Sliding mode control;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2015 34th Chinese
Conference_Location
Hangzhou, China
Type
conf
DOI
10.1109/ChiCC.2015.7260146
Filename
7260146
Link To Document