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控制力矩陀螺框架高精度周期随动控制

徐向波 李海涛 薛立娟 杨莲慧

徐向波, 李海涛, 薛立娟, 等 . 控制力矩陀螺框架高精度周期随动控制[J]. 北京航空航天大学学报, 2012, 38(8): 1017-1021.
引用本文: 徐向波, 李海涛, 薛立娟, 等 . 控制力矩陀螺框架高精度周期随动控制[J]. 北京航空航天大学学报, 2012, 38(8): 1017-1021.
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)
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)

控制力矩陀螺框架高精度周期随动控制

基金项目: 国家973计划资助项目(2009CB724000)
详细信息
  • 中图分类号: TP 271

High precision periodic control method of control moment gyro gimbal system

  • 摘要: 为实现控制力矩陀螺框架伺服系统的高精度周期随动控制,采用比例积分微分(PID,Proportion Integration Differentiation)控制器结合重复控制器的控制方式,PID控制器实现框架伺服系统静态和匀速运动的高精度控制,插入式重复控制器实现对周期性输入信号的精确跟踪.对控制力矩陀螺框架系统进行了建模,设计了PID控制器与插入式重复控制器,并分析了重复控制器的稳定性条件、稳态跟踪性能和对扰动的抑制能力.仿真结果和实验结果表明:采用插入式重复控制器使控制力矩陀螺跟踪1Hz给定速度信号时的稳态跟踪误差大幅减少.PID控制器结合插入式重复控制器结构简单,两者可分开独立设计,参数设计容易.

     

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出版历程
  • 收稿日期:  2011-05-13
  • 网络出版日期:  2012-08-30

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