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航天器编队飞行多目标姿态快速跟踪鲁棒控制

袁长清 李俊峰 王天舒 宝音贺西

袁长清, 李俊峰, 王天舒, 宝音贺西. 航天器编队飞行多目标姿态快速跟踪鲁棒控制[J]. 应用数学和力学, 2008, 29(2): 169-180.
引用本文: 袁长清, 李俊峰, 王天舒, 宝音贺西. 航天器编队飞行多目标姿态快速跟踪鲁棒控制[J]. 应用数学和力学, 2008, 29(2): 169-180.
YUAN Chang-qing, LI Jun-feng, WANG Tian-shu, BAOYIN He-xi. Robust Attitude Control for Rapid Multi-Target Tracking in Spacecraft Formation Flying[J]. Applied Mathematics and Mechanics, 2008, 29(2): 169-180.
Citation: YUAN Chang-qing, LI Jun-feng, WANG Tian-shu, BAOYIN He-xi. Robust Attitude Control for Rapid Multi-Target Tracking in Spacecraft Formation Flying[J]. Applied Mathematics and Mechanics, 2008, 29(2): 169-180.

航天器编队飞行多目标姿态快速跟踪鲁棒控制

基金项目: 国家自然科学基金资助项目(10672084);高等学校博士学科点专项科研基金资助项目(20060003097)
详细信息
    作者简介:

    袁长清(1974- ),男,博士生(Tel:+86-10-62773402;E-mail:ycq02@mails.tsinghua.edu.cn);王天舒,男,副教授,博士(联系人.Tel:+86-10-62773402;E-mail:tswang@tsinghua.edu.cn).

  • 中图分类号: V412.4

Robust Attitude Control for Rapid Multi-Target Tracking in Spacecraft Formation Flying

  • 摘要: 研究了航天器编队飞行多目标姿态跟踪鲁棒控制问题.主航天器装有一个快速机动天线和一个星载相机.考虑相机对地面目标跟踪,同时考虑天线与从航天器通信的空间任务.通过引入角速度约束和姿态角约束,分别推导了相机和天线的参考姿态角、角速度和角加速度.提出期望逆系统的概念,将三维空间姿态跟踪问题转化为调节问题,简化了控制器的设计.考虑存在参数摄动和外部干扰力矩的情况,基于期望逆系统和滑模控制,设计了鲁棒姿态跟踪控制器,并利用Liapunov稳定性理论证明了控制系统的渐近稳定性.以两航天器编队飞行多目标跟踪为例进行数值仿真,结果表明所设计的控制器具有良好的鲁棒性和优越的跟踪性能.
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出版历程
  • 收稿日期:  2007-01-17
  • 修回日期:  2008-01-02
  • 刊出日期:  2008-02-15

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