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Volume 38 Issue 8
Aug.  2012
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Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  38(8): 1017-1021.
Zhang Mingchuan, Zhang Jin, Tang Diyiet al. Analysis of Axial-Flow Compressors Stall in Uniform and Distorted Inlet Flow[J]. Journal of Beijing University of Aeronautics and Astronautics, 1998, 24(6): 704-706. (in Chinese)
Citation: Xu Xiangbo, Li Haitao, Xue Lijuan, et al. High precision periodic control method of control moment gyro gimbal system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(8): 1017-1021. (in Chinese)
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High precision periodic control method of control moment gyro gimbal system

  • School of Instrument Science and Opto-electronics Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 13 May 2011
  • Publish Date: 30 Aug 2012
    Abstract
  • In order to realize high periodic precision control of control moment gyro (CMG) gimbal system, a controller consisted of proportiona integration differention (PID) controller and plug-in repetitive controller was adopted. PID controller can realize high precision control of static state and uniform speed state, while plug-in repetitive controller can realize accurate tracking of periodic given signal. CMG gimbal system modeling was performed, and the PID controller and plug-in repetitive controller were designed, then stability conditions, steady tracking properties and ability of suppressing disturbance were analyzed. Simulation and experiment results show plug-in repetitive controller can effectively reduce steady tracking error when CMG gimbal system tracks a 1Hz periodic given velocity signal. The structure of the controller is simple and the plug-in repetitive controller can be designed separated from system’s PID controller, so it is easy to design parameters.

     

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    • References(11)
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