Relative orbit and attitude coupled control algorithm design based on compound control for autonomou

来源 :The 4th International Conference on Dynamics, Vibration and | 被引量 : 0次 | 上传用户：ccbone

【摘要】

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【作者】

：

Wei Lu Xueyan An Xiaotao Yan

【机构】

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Beijing Institute of Astronautical Systems Engineering, Beijing China, 100076

【出处】

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The 4th International Conference on Dynamics, Vibration and

【发表日期】

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2014年8期

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In the mission of on-orbit rescuing an out-of-control target, the servicing spacecraft needs autonomous rendezvous and dock to the out-of-control target.In such mission, the position of out-of-control target s docking port is changing with time as the result of the out-of-control target s attitude tumbling in space.And the servicing spacecraft s docking port should point to the out-of-control target s docking port when two spacecrafts docking.

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