Volume 34 Issue 1
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Article Navigation >  Chinese Journal of Space Science  > 2014  >  34(1): 109-115
HUANG Yong, LI Xiaojiang, WANG Zhiheng, LI Zhaoming. Finite-time Control of Satellites Formation[-1.5mm] Based on Terminal Sliding Mode[J]. Chinese Journal of Space Science, 2014, 34(1): 109-115. doi: 10.11728/cjss2014.01.109
Citation: HUANG Yong, LI Xiaojiang, WANG Zhiheng, LI Zhaoming. Finite-time Control of Satellites Formation[-1.5mm] Based on Terminal Sliding Mode[J]. Chinese Journal of Space Science, 2014, 34(1): 109-115. doi: 10.11728/cjss2014.01.109
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Finite-time Control of Satellites Formation[-1.5mm] Based on Terminal Sliding Mode

doi: 10.11728/cjss2014.01.109

  • Company of Postgraduate Management, the Academy of Equipment, Beijing 101416

  • Received Date: 2013-06-19
  • Rev Recd Date: 2013-11-11
  • Publish Date: 2014-01-15
    Abstract
  • Aiming at the relative control problem of reference satellite maneuver-considered formation flying, a finite-time control method based on terminal sliding mode (TSM) is given. Based on the dynamic model of formation satellites relative motion, a finite-time terminal sliding controller is designed, and it is proven that the system state error can converge in finite time under the controller. Lastly, the formation reconfiguration and the formation keeping considering reference satellite maneuver are simulated and analyzed with the control method. The results show that the finite-time control method based on terminal sliding mode has higher formation control precision as well as faster error convergence speed compared with the traditional linear sliding mode.

     

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