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挠性卫星的自适应模糊滑模控制 被引量:8

The Adaptive Fuzzy Sliding Mode Control for Flexible Satellite
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摘要 将自适应模糊滑模控制应用于挠性卫星的姿态稳定控制中 ,给出了详尽的实现方法。用一个自适应模糊控制器逼近滑模控制中的等效控制 ,推导了规则参数调整的自适应率 ,确定不连续控制以保证闭环控制系统的稳定性 ,用另一个模糊控制器光滑不连续控制以抑制抖振。仿真结果表明 ,该方法实现了较高精度的卫星姿态控制。 In this paper,the adaptive fuzzy s li ding mode control is applied to the attitude stabilization of flexible satellite ,and the detailed design procedure of the fuzzy sliding mode control system is p resented. The adaptive fuzzy control is utilized to approach the equivalent cont rol of sliding mode control,then the adaptive law is derived. The discontinuous control, which guarantees the stability of control system, is developed. Also in order to attenuate the chattering phenomena, another fuzzy controller is employ ed to smooth the discontinuous control.Simulation results show that precise atti tude control is accomplished based on the proposed method.
作者 管萍 陈家斌
出处 《航天控制》 CSCD 北大核心 2004年第4期62-67,共6页 Aerospace Control
基金 国防预研基金资助项目 (5 14 0 90 80 2 0 )
关键词 自适应模糊控制 滑模控制 姿态控制 挠性卫星 Subject terms Adaptive fuzzy control Sliding mode control Attitude control Flexible satelli te
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参考文献6

  • 1Chen Y P, Lo S C. Sliding - mode controller design for spacecraft attitude tracking maneuvers [ J ]. IEEE Transactions on Aerospace and Electronic Systems, 1993,29(4) :1328 - 1333
  • 2Karray F, Modi V. On the pointing robustness issue of a class of new generation spacecraft[J]. IEEE Transactions on Automatic Control, 1995, 40(12) :2132 -2137
  • 3Jovan D B, Li S M, Raman K M. Robust adaptive variable structure control of spacecraft under control input saturation[ J]. Journal of Guidance, Control and Dynamics,2001,24( 1 ): 14 - 22
  • 4Hwang G C, Chang S. A stability approach to fuzzy control design for nonlinear system[ J]. Fuzzy Sets and Systems. 1992, 48:279-287
  • 5Rainer P. Robust control by fuzzy sliding mode. Automatica[J] , 1994, 30(9) :1429 - 1437
  • 6王青,胡昌华.柔性空间结构的分散模糊变结构控制[J].宇航学报,2000,21(1):23-27. 被引量:6

二级参考文献4

共引文献5

同被引文献65

  • 1张云,王培垣.一种用于挠性卫星姿态控制的改进模糊控制器[J].上海航天,2004,21(6):42-45. 被引量:2
  • 2王蜀泉,尹逊和,赵光恒.用于卫星姿态机动控制的一种自适应模糊控制器[J].空间科学学报,2006,26(1):54-58. 被引量:3
  • 3胡庆雷,马广富.带有输入非线性的挠性航天器姿态机动变结构控制[J].宇航学报,2006,27(4):630-634. 被引量:17
  • 4黄圳圭.航天姿态动力学[M].长沙:国防科技大学出版社,2006.
  • 5PASSION K M,YURKOVICH S.Fuzzy control[M].Indianapolis:Addison Wesley Longman Inc.,1998.
  • 6AHMED J,COPPOLA J,BERNSTEIN D S.Adaptive asymptotic tracking of spacecraft attitude motion with inertia matrix identification[J].Journal of Guidance Control and Dynamics,1998,21(5):684-691.
  • 7WONG H,QUEIROZ M S,KAPILA V.Adaptive tracking control using synthesized velocity from attitude measurements[J].Automatica,2001,37(6):947-953.
  • 8COSTIC B T,DAWSON D M,KAPILA V Quaternion-based adaptive attitude tracking controller without velocity measurements[J].Journal of Guidance Control and Dynamics,2001,24(6):1214-1222.
  • 9CAI W C,LIAO X H,SONG Y D.Indirect robust adaptive faulttolerant control for attitude tracking of spacecraft[J].Journal of Guidance Control and Dynamics,2008,31(5):1456-1463.
  • 10JIN E D,SUN Z W.Robust controllers design with finite titre convergence for rigid spacecraft attitude tracking control[J].Aerospace Science and Technology,2008,12(4):324-330.

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