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�������պ����ѧѧ�� 2000, Vol. 26 Issue (5) :509-512    DOI:
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Decoupling Sliding Mode Control in A Nonlinear Spacecraft System
ZHU Min-xiong1, SONG Yi2, SONG Chao-qing2*
1. Beijing University of Aeronautics and Astronautics,Dept. of Automatic Control;
2. China Academy of Launch Vehicle Technology

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Abstract�� A control method with sliding mode of nonlinear spacecraft system is provided in this paper, in which the interactive influences among channels of strong nonlinear spacecraft system are decoupled. The decoupled spacecraft with large parameter variations and external disturbances is of good robustness. The numerical simulations of its attitude stability and maneuver control give support to the effectiveness of results in this paper.
Keywords�� reentry vehicles   attitude control systems   non-linear systems   sliding mode control     
Received 1999-04-09;
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ZHU Min-xiong, SONG Yi, SONG Chao-qing.Decoupling Sliding Mode Control in A Nonlinear Spacecraft System[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2000,V26(5): 509-512
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2000/V26/I5/509
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