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基于迭代学习观测器的卫星姿态控制系统的鲁棒容错控制 被引量:13

Robust Fault-Tolerant Control for Satellite Attitude Control System Based on Iterative Learning Observer
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摘要 针对卫星在轨运行时存在执行机构故障和空间干扰问题,提出了一种将迭代学习与未知输入观测器(IL-UIO)相结合的鲁棒容错控制方法。该方法在继承了未知输入观测器干扰解耦优点的同时,运用迭代学习技术,利用前一时刻姿态角速度偏差和IL-UIO输入来更新当前故障信息,实现了执行机构的在线故障重构。进一步基于Lyapunov方法从理论上证明了设计的IL-UIO鲁棒稳定性和姿态角速度偏差一致有界性。最后,建立卫星闭环姿态控制系统对方法进行验证,仿真结果验证了方法的有效性。 Based on Iterative learning-unknown input observer ( IL-UIO ), a robust fault-tolerant control scheme is pufford to deal with actuator failures and external disturbances of on-orbit satellite. It decouples disturbances with UIO, meanwhile the IL technique are used to update current fault signal by means of immediate past system output errors and the last step IL-UIO information, thus reconstructing actuator fault on-line. Furthermore, the robust stability of the full-order IL-UIO and uniformly boundness of angular velocity errors are proved by using the Lyapunov stability theory. Simulation results of the closed-loop satellite attitude control system used in a satellite attitude control system validate the effectiveness of the proposed method.
出处 《宇航学报》 EI CAS CSCD 北大核心 2012年第8期1080-1086,共7页 Journal of Astronautics
基金 国家自然科学基金(60874054)
关键词 迭代学习 未知输入观测器 故障重构 鲁棒容错控制 卫星姿控系统 Iterative learning Unknown input observer Fault reconstruction Robust fault-tolerant control Satelliteattitude control system
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  • 1杜永昌,管迪华,宋健.汽车道路模拟算法研究[J].公路交通科技,2001,18(6):115-118. 被引量:15
  • 2刘莹莹,周军.挠性多体航天器姿态动力学建模与分析[J].飞行力学,2005,23(3):60-63. 被引量:12
  • 3吴继轩,刘向东.高频角振动测试转台的迭代学习控制[J].计算机仿真,2005,22(11):307-310. 被引量:5
  • 4栾家辉,姜兴渭,宋政吉.干扰解耦降维观测器设计的新方法[J].南京理工大学学报,2006,30(3):306-310. 被引量:3
  • 5陈雪芹,耿云海,张世杰,张迎春.基于混合H_2H_∞的集成故障诊断与容错控制研究[J].宇航学报,2007,28(4):890-896. 被引量:12
  • 6Chen R H, Speyer J L. Sensor and actuator fault reconstruction [ J]. Journal of Guidance Control and Dynamics, 2004, 27 (2) :186 -196.
  • 7Jiang T, Khorasani K. A fault detection, isolation and recon- struction strategy for a satellitek' s attitude control subsystem with redundant reaction wheels[ C ]. IEEE International Conference on Systems, Man and Cybernetics, Montreal, Cook Islands, October 7-10, 2007.
  • 8Curry T D, Collins E G. Robust fauh detection and isolation using robust 12 estimation [ J]. Journal of Guidance Control and Dynamics, 2005, 28(6): 1131 -1139.
  • 9Hou Q, ChengY H, Lu N Y, JiangB. Study on FDD and FTC of satellite attitude control system based on the effectiveness factor [ C ]. The 2nd International Symposium on Systems and Control in Aerospace and Astronautics, Shenzhen, China. Dec 10 - 12, 2008,.
  • 10Henry D. Fault diagnosis of microscope satellite thrusters using H - infinity/H-filters[ J]. Journal of Guidance Control and Dynamics, 2008, 31(3): 699-711.

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