DocumentCode :
3056091
Title :
Spacecraft attitude stabilization using optimal sliding mode control
Author :
Li, Chuanjiang ; Wang, Yibo ; Xu, Liang ; Zhang, Zhongzhao
Author_Institution :
Control Sci. & Eng. Dept., Harbin Inst. of Technol., Harbin, China
fYear :
2010
fDate :
8-10 June 2010
Firstpage :
1085
Lastpage :
1089
Abstract :
The attitude stabilization problem for a spacecraft is addressed through the combination of optimal control and sliding mode variable structure control method. We first determine an optimal sliding manifold for the kinematical subsystem of the spacecraft. Then a variable structure controller, which is based on equivalent control and the optimal sliding surface, is designed for the whole dynamical and kinematical system. An important feature of the methodology is that when the sliding manifold is reached, the attitude variables will be stabilized to the origin in the sense of optimality with respect to a quadratic cost functional. The proposed controller is also robust to external disturbances. Simulations are performed to demonstrate the effectiveness of the proposed optimal sliding mode controller.
Keywords :
attitude control; optimal control; robust control; space vehicles; variable structure systems; attitude variable; dynamical system; external disturbance; kinematical subsystem; kinematical system; optimal sliding manifold; optimal sliding mode control; optimal sliding surface; quadratic cost functional; robust control; sliding mode variable structure control; spacecraft attitude stabilization; Aerodynamics; Angular velocity; Attitude control; Manifolds; Materials requirements planning; Optimal control; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location :
Harbin
Print_ISBN :
978-1-4244-6043-4
Electronic_ISBN :
978-1-4244-7505-6
Type :
conf
DOI :
10.1109/ISSCAA.2010.5633998
Filename :
5633998
Link To Document :
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