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存在飞轮安装偏差与故障的卫星姿态容错控制

DOI: 10.13195/j.kzyjc.2013.0807, PP. 1434-1438

Keywords: 卫星,安装偏差,部分失效故障,容错控制,有限时间

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Abstract:

基于滑模控制理论提出一种刚体卫星姿态稳定控制方法,实现对反作用飞轮部分失效故障的容错控制,以及对其安装偏差的补偿控制,并从理论上证明了所设计的控制器在有限时间内能够实现对闭环姿态控制系统的几乎全局渐近稳定控制.最后将所设计的控制器应用于某型卫星姿态稳定任务,仿真结果验证了所提出方法的有效性.

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