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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.
  • [1] Gramling C J, Taesul Lee, Niklewski D J,et al.Relative navigation for autonomous formation flying of spacecraft[A].In:Proceedings of the 1997 AAS/AIAA Astrodynamics Spcialist Conference[C].Colorado:AAS Pblications Office,1997,435-450.
    [2] DeCou A B. Orbital station-keeping for multiple spacecraft interferometry[J].Journal of the Astronautical Sciences,1991,39(3):283-297.
    [3] David J I. A study of linear vs nonlinear control techniques for the reconfiguration of satellite formations[D].Ph D Dissertation.Dayton:Air Force Institute of Technology,Air University, 2001.
    [4] LIU Hui, LI Jun-feng.Sliding mode control for low-thrust earth-orbiting spacecraft formation maneuvering[J].Aerspace Science and Technology,2006,10(6):636-643. doi: 10.1016/j.ast.2006.04.008
    [5] Hablani H B. Design of a payload pointing control system for tracking moving objects[J].Journal of Guidance, Control, and Dynamics,1989,12(3):365-374. doi: 10.2514/3.20417
    [6] Hablani H B. Multiaxis Tracking and attitude-control of flexible spacecraft with reaction jets[J].Journal of Guidance Control and Dynamics,1994,17(4):831-839. doi: 10.2514/3.21273
    [7] 李俊峰, 徐敏, Steyn W H.低轨道航天器姿态跟踪机动研究[J].清华大学学报(自然科学版),2001,41(2):102-104.
    [8] Ren W, Beard R W. Formation feedback control for multiple spacecraft via virtural structures[J].IEE Proc Control Theory Appl,2004,151(3):357-368. doi: 10.1049/ip-cta:20040484
    [9] Matthew C V, Christopher D H.Decentralized coordinated attitude control within a formation of spacercraft[J].Journal of Guidance, Control and Dynamics,2006,29(5):1101-1109. doi: 10.2514/1.17857
    [10] Matthew R L. Spacecraft attitude tracking control[D].M Sc Dissertation.Blacksburg:The Virginia Polyechnic Institute and State University,1999.
    [11] Shuster M D. A survey of attitude representations[J].Journal of the Astronautical Sciences,1993,41(4):439-517.
    [12] Unwin M J,Oldfield M K. Preliminary orbital result from the SGR space GPS receiver[A].In:Proc ION GPS-99[C].Nashville,Sep,1999,849-856.
    [13] 李春文, 冯元琨.多变量非线性控制的逆系统方法[M].北京:清华大学出版社, 1991.
    [14] CHEN Yon-ping.Sliding-mode controller design for spacecraft attitude tracking maneuvers[J].IEEE Transactions on Aerospace and Electronic Systems,1993,29(4):1328-1333. doi: 10.1109/7.259536
    [15] Goeree B B, Fasse E D. Sliding mode attitude control of a small satellite for ground tracking maneuvers[A].In:2000 American Control Conferece,Jun 28-30,Chicago,IL.Proceedings of the American Control Conference[C].2000,1134-1138.
    [16] FENG Yong, YU Xing-huo. Non-singular terminal sliding mode control of rigid manipulators[J].Automatica,2002,38(12):2159-2167. doi: 10.1016/S0005-1098(02)00147-4
    [17] JING Wu-xing,XU Shi-jie.Nonlinear Attitude tracking control of a spacecraft with thrusters based on error quaternions[J].Chinese Journal of Aeronautics,2002,15(3):129-138. doi: 10.1016/S1000-9361(11)60142-8
    [18] Tang C. Adaptive nonlinear attitude control of spacecraft[D].Ph D Dissertation.Ames:Iowa State University, 1995.
    [19] LUO Wen-cheng,CHU Yun-chung. Hinf tracking control of a rigid spacecraft [A].In:Proceedings of the American Control Conferenceg[C].July,2004,2681-2686.
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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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