DocumentCode :
1859764
Title :
Robust fault tolerant attitude stabilization control for flexible spacecraft under partial loss of actuator effectiveness
Author :
Hu, Qinglei ; Xiao, Bing ; Zhang, Youmin
Author_Institution :
Dept. of Control Sci. & Eng., Harbin Inst. of Technol., Harbin, China
fYear :
2010
fDate :
6-8 Oct. 2010
Firstpage :
263
Lastpage :
268
Abstract :
Robust fault tolerant attitude stabilization control problem for flexible spacecraft is investigated in this paper. First, a robust controller based on sliding mode control scheme is derived, in which function approximation technique is employed to represent system uncertainties. It is shown that the roll angle, pitch angle and yaw angle can be globally asymptotically stabilized in the presence of bounded disturbances and partial loss of actuator effectiveness fault. Moreover, adaptive scheme is employed to estimate the uncertain bound of actuator fault such that the real bound value of the fault is not used in advance for the designers. Complete stability and performance analysis are presented and illustrative simulation results of application to a spacecraft show that high precise attitude control is successfully achieved in the presence of various scenarios of control effect failures.
Keywords :
actuators; asymptotic stability; attitude control; fault tolerance; robust control; space vehicles; variable structure systems; actuator effectiveness; asymptotic stability; flexible spacecraft; function approximation technique; pitch angle; robust fault tolerant attitude stabilization control; roll angle; sliding mode control scheme; yaw angle; Actuators; Attitude control; Fault tolerance; Fault tolerant systems; Space vehicles; Stability analysis; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Fault-Tolerant Systems (SysTol), 2010 Conference on
Conference_Location :
Nice
Print_ISBN :
978-1-4244-8153-8
Type :
conf
DOI :
10.1109/SYSTOL.2010.5676037
Filename :
5676037
Link To Document :
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