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存在飞轮安装偏差与故障的卫星姿态容错控制 被引量：1

Satellite attitude fault tolerant control with reaction wheel misalignment and fault
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摘要 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. An attitude stabilization scheme is presented for a rigid satellite. The partial loss of reaction wheel effectiveness is tolerated, and reaction wheel misalignment is also compensated. The Lyapunov stability analysis shows that the closed-loop attitude system is guaranteed to be almost asymptotically stable in finite-time. An illustrative example of a satellite is given, and simulation results show the effectiveness of the derived control law.
作者 霍星 胡庆雷 肖冰
机构地区 哈尔滨工业大学控制科学与工程系 渤海大学工学院
出处 《控制与决策》 EI CSCD 北大核心 2014年第8期1434-1438,共5页 Control and Decision
基金 国家自然科学基金项目(61273175) 辽宁省自然科学基金项目(2013020044)
关键词 卫星 安装偏差 部分失效故障 容错控制 有限时间 satellite actuator misalignment partial loss of effectiveness fault tolerant control finite time
分类号 V448.22 [航空宇航科学与技术—飞行器设计]
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参考文献15

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二级参考文献45

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控制与决策
2014年 第8期

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