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充液航天器大角度机动自适应无源控制

王宏伟 宋晓娟 李长杰

王宏伟, 宋晓娟, 李长杰. 充液航天器大角度机动自适应无源控制[J]. 空间科学学报, 2020, 40(3): 408-418. doi: 10.11728/cjss2020.03.408
引用本文: 王宏伟, 宋晓娟, 李长杰. 充液航天器大角度机动自适应无源控制[J]. 空间科学学报, 2020, 40(3): 408-418. doi: 10.11728/cjss2020.03.408
WANG Hongwei, SONG Xiaojuan, LI Changjie. Adaptive Passive Control for Large-angle Attitude Maneuver of Liquid-filled Spacecraft[J]. Journal of Space Science, 2020, 40(3): 408-418. doi: 10.11728/cjss2020.03.408
Citation: WANG Hongwei, SONG Xiaojuan, LI Changjie. Adaptive Passive Control for Large-angle Attitude Maneuver of Liquid-filled Spacecraft[J]. Journal of Space Science, 2020, 40(3): 408-418. doi: 10.11728/cjss2020.03.408

充液航天器大角度机动自适应无源控制

doi: 10.11728/cjss2020.03.408
基金项目: 

国家自然科学基金项目(11962020,11862020,11502122)和内蒙古自然科学基金项目(2019MS05065)共同资助

详细信息
    作者简介:

    宋晓娟,E-mail:xjsong0603@163.com

  • 中图分类号: V448

Adaptive Passive Control for Large-angle Attitude Maneuver of Liquid-filled Spacecraft

  • 摘要: 研究了基于自适应无源控制的三轴稳定充液航天器大角度姿态机动问题.将液体晃动等效为黏性球摆模型,利用动量矩守恒定理推导出充液航天器耦合动力学方程.针对陀螺故障及无陀螺配置导致航天器姿态无角速度测量的情况,同时考虑存在外部未知干扰、转动惯量不确定性以及液体晃动位移不可测量的特性,设计自适应输出反馈无源控制,其中自适应更新律用于补偿外部未知干扰和估计液体晃动的位移变量.利用Lyapunov方法和LaSalle不变引理,证明该控制律不但可以保证闭环系统渐进稳定,而且可以保证二个期望平衡位置均达到稳定.仿真结果验证了本文控制方法的有效性.

     

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出版历程
  • 收稿日期:  2019-03-06
  • 修回日期:  2020-02-11
  • 刊出日期:  2020-05-15

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