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Volume 26 Issue 5
May  2000
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Journal of Beijing University of Aeronautics and Astronautics  > 2000  >  26(5): 509-512.
ZHU Min-xiong, SONG Yi, SONG Chao-qinget al. Decoupling Sliding Mode Control in A Nonlinear Spacecraft System[J]. Journal of Beijing University of Aeronautics and Astronautics, 2000, 26(5): 509-512. (in Chinese)
Citation: ZHU Min-xiong, SONG Yi, SONG Chao-qinget al. Decoupling Sliding Mode Control in A Nonlinear Spacecraft System[J]. Journal of Beijing University of Aeronautics and Astronautics, 2000, 26(5): 509-512. (in Chinese)
shu

Decoupling Sliding Mode Control in A Nonlinear Spacecraft System

  • 1.

    Beijing University of Aeronautics and Astronautics,Dept. of Automatic Control

  • 2. China Academy of Launch Vehicle Technology

  • Received Date: 09 Apr 1999
  • Publish Date: 31 May 2000
    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.

     

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    • References(1)
  • [1]徐延万.控制系统(上)[M].北京:宇航出版社,1989. [2]Hedrick J K. Analysis and control of nonlinear systems[J]. Journal of Dynamic Systems, Measurement and Control, 1993,115:351~361. [3]Gao W B, Hung J C. Variable structure control of nonlinear systems, a new approach[J]. IEEE Trans Ind Electron, 1993,40(1):44~45. [4]Sira-Ramirez H. On the dynamical sliding mode control of nonlinear systems[J].INT J Control, 1993,57(5):1039~1061.
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