DocumentCode :
724068
Title :
Attitude stabilization of flexible satellite subject to external disturbance and actuator constraint
Author :
Aihua Zhang ; Haitao Meng ; Zhiqiang Zhang ; Xing Huo
Author_Institution :
Coll. of Eng., Bohai Univ., Jinzhou, China
fYear :
2015
fDate :
23-25 May 2015
Firstpage :
1558
Lastpage :
1563
Abstract :
This work presents a nonlinear control approach to address the problem of attitude stabilization for flexible satellite. Actuator constraint and unknown external disturbance are explicitly considered. Firstly, a backstepping based control law is proposed in the absence of actuator constraint. It guarantees that the attitude and the angular velocity are asymptotic stable even in the presence of unknown appendage´s vibration and disturbance. Take actuator constraint into account, another backstepping based controller is then developed. It shows that the closed-loop attitude system is uniformly ultimately bounded. Simulation results are also presented to demonstrate the effectiveness of the proposed scheme.
Keywords :
actuators; asymptotic stability; attitude control; closed loop systems; control nonlinearities; nonlinear control systems; actuator constraint; angular velocity; asymptotic stability; attitude stabilization; backstepping based control law; closed-loop attitude system; flexible satellite; nonlinear control approach; unknown appendage vibration; unknown external disturbance; Actuators; Angular velocity; Attitude control; Backstepping; Satellites; Torque; Vibrations; Actuator constraint; Attitude stabilization; Backstepping;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Decision Conference (CCDC), 2015 27th Chinese
Conference_Location :
Qingdao
Print_ISBN :
978-1-4799-7016-2
Type :
conf
DOI :
10.1109/CCDC.2015.7162167
Filename :
7162167
Link To Document :
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