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基于极点配置的空间站角动量管理

党庆庆 金磊 徐世杰

党庆庆, 金磊, 徐世杰等 . 基于极点配置的空间站角动量管理[J]. 北京航空航天大学学报, 2016, 42(8): 1715-1723. doi: 10.13700/j.bh.1001-5965.2015.0535
引用本文: 党庆庆, 金磊, 徐世杰等 . 基于极点配置的空间站角动量管理[J]. 北京航空航天大学学报, 2016, 42(8): 1715-1723. doi: 10.13700/j.bh.1001-5965.2015.0535
DANG Qingqing, JIN Lei, XU Shijieet al. Angular momentum management of space station based on pole placement[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(8): 1715-1723. doi: 10.13700/j.bh.1001-5965.2015.0535(in Chinese)
Citation: DANG Qingqing, JIN Lei, XU Shijieet al. Angular momentum management of space station based on pole placement[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(8): 1715-1723. doi: 10.13700/j.bh.1001-5965.2015.0535(in Chinese)

基于极点配置的空间站角动量管理

doi: 10.13700/j.bh.1001-5965.2015.0535
基金项目: 国家自然科学基金(11272027)
详细信息
    作者简介:

    党庆庆,男,硕士研究生。主要研究方向:导航制导与控制。Tel.:010-82339750。E-mail:dangqingqingbuaa@163.com;金磊,女,博士,副教授,硕士生导师。主要研究方向:航天器姿态动力学与控制。Tel.:010-82339750。E-mail:jinleibuaa@163.com

    通讯作者:

    金磊,Tel.:010-82339750,E-mail:jinleibuaa@163.com

  • 中图分类号: V221+.3;TB553

Angular momentum management of space station based on pole placement

  • 摘要: 针对惯性系下引力梯度力矩及其他干扰力矩引起控制力矩陀螺(CMG)角动量积累的问题,采用引力梯度力矩来平衡姿态,设计了基于极点配置的空间站角动量管理控制器。首先在惯性系下建立了空间站线性化模型,并分析了俯仰轴方向在惯性系角动量管理的不可行性。由此,将俯仰轴与滚动/偏航轴解耦,不约束俯仰轴方向的CMG角动量,将常值、1倍和2倍于轨道频率的扰动纳入状态方程以抑制其对俯仰轴姿态的影响。在滚动/偏航轴方向将常值扰动纳入状态方程中以抑制其对CMG角动量的影响;将1倍、2倍于轨道频率的扰动纳入到状态方程中以抑制其对姿态的影响。然后采用带极点配置的线性二次型(LQR)算法求解出反馈增益矩阵,该算法可以避免选取权重矩阵,并且根据系统性能要求即能将闭环极点配置到复平面虚轴左侧指定的区域。最后仿真结果验证了该算法的可行性。

     

  • [1] WIE B,BYUN K,WARREN V,et al.New approach to attitude/momentum control for the space station[J].Journal of Guidance,Control,and Dynamices,1988,12(5):714-722.
    [2] PARLOS A G,SUNKEL J W.Adaptive stability and control for space station/orbiter berthing operations:AIAA-1992-4480[R].Reston:AIAA,1992.
    [3] PARLOS A G,SUNKEL J W.Adaptive control and momentum management for large-angle spacecraft maneuvers[J].Journal of Guidance,Control,and Dynamices,1992,15(4):1018-1028.
    [4] PARLOS A G,SUNKEL J W.Attitude control/momentum management of the space station freedom for large angle torque-equilibrium-attitude configurations:AIAA-1990-3352[R].Reston:AIAA,1990.
    [5] HARDUVEL J T. Continuous momentum management of earth-orbited spacecraft[J].Journal of Guidance,Control,and Dynamices,1992,15(6):1417-1426.
    [6] 朱孟萍,徐世杰,陈新龙,等.基于参数辨识的大型航天器自适应角动量管理[J].空间控制技术与应用,2014,40(3):47-52.ZHU M P,XU S J,CHEN X L,et al.Adaptive momentum management of large spacecraft based on parameter identification[J].Aerospace Control and Application,2014,40(3):47-52(in Chinese).
    [7] ZHU M P,XU S J.Stability-based SDRE controller for spacecraft momentum management[J].Acta Astronautica,2013,89:71-82.
    [8] XIN M,BALAKRSHNAN S N.A new method for suboptimal control of a class of nonlinear systems[C]//41st IEEE Conference on Decision and Control. Piscataway,NJ:IEEE Press,2002:2756-2761.
    [9] SHIEH S L,DIB M H,GANESAN S.Linear quadratic regulators with eigenvalue placement in a specified region[J].Automatica,1988,24(6):819-823.
    [10] SHIEH S L,DIB M H,GANESAN S.Continuous-time quadratic regulators and pseudo-continuous-time quadratic regulators with pole placement in a specific region[J]. IEEE Proceedings D-Control Theory and Applications,1987,134(5):338-346.
    [11] SHIEH S L,DIB M H,GANESAN S.Linear quadratic regulators with eigenvalue placement in a vertical strip[J].IEEE Transaction on Automatic Control,1986,31(3):241-243.
    [12] KOSHKOUEI A J,ZINDOBER A S I.Comment on "linear quadratic regulators with eigenvalue placement in a vertical strip"[J].IEEE Transactions on Automatic Control,1999,44(7):1417-1419.
    [13] SUNKEL J W,SHIEH L S,ZHANG J L.Digital redesign of an optimal momentum mangement controller for the space station[J].Journal of Guidance,Control,and Dynamices,1991,14(4):712-723.
    [14] SUNKEL J W,SHIEH L S.Multistage design of an optimal momentum management controller for the space station[J].Journal of Guidance,Control,and Dynamices,1991,14(3):492-502.
    [15] 张军,马艳红,何英姿.空间站组合体惯性系内角动量管理控制[J].空间控制技术与应用,2010,36(6):1-5.ZHANG J,MA Y H,HE Y Z.Momentum management control of space station complex in intertial reference[J].Aerospace Control and Application,2010,36(6):1-5(in Chinese).
    [16] 张洪华,吴宏鑫,陈义庆.挠性卫星姿态的角动量反馈控制[J].宇航学报,2002,23(3):8-12.ZHANG H H,WU H X,CHENG Y Q.Angular momentum feedback control for flexible spacecraft[J].Journal of Astronautics,2002,23(3):8-12(in Chinese).
    [17] KAWASAKI N,SHIMEMURA E.Determining quadratic weighting matrices to locate poles in a specified region[J].Automatica,1983,19(5):557-560.
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出版历程
  • 收稿日期:  2015-08-24
  • 刊出日期:  2016-08-20

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