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旋转非合作目标终端逼近的姿轨控制研究

DOI: 10.11728/cjss2015.05.603, PP. 603-610

Keywords: 相对运动,非合作目标,空间交会,轨道控制,姿态控制

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Abstract:

针对旋转非合作目标的终端逼近过程进行研究,建立了适用于任意偏心率的精确航天器相对运动和姿态动力学模型,并对传统的直线型同步自旋逼近策略进行改进,设计了用于保障终端逼近安全性的指数衰减型参考轨迹;推导了基于比例微分加解耦控制方法的相对轨道和姿态控制律,通过数值仿真验证了控制器的有效性.

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