Low-complexity Stabilization Control of Combined Spacecraft with an Unknown Captured Object

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• 英文论文题名：Low-complexity Stabilization Control of Combined Spacecraft with an Unknown Captured Object
• 论文作者：Caisheng Wei ; Jianjun Luo ; Chen Xu ; Jianping Yuan
• 英文论文作者：Caisheng Wei ; Jianjun Luo ; Chen Xu ; Jianping Yuan ; National Key Laboratory of Aerospace Flight Dynamics ; Northwestern Polytechnical University
• 年：2017
• 作者机构：National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University;
• 英文论文关键词：Nonlinear Control ; Prescribed Performance ; Spacecraft ; Non-cooperative Target
• 会议召开时间：2017-07-26
• 会议录名称：第36届中国控制会议论文集（A）
• 英文会议录名称：Proceedings of the 36th Chinese Control Conference（A）
• 语种：英文
• 分类号：V448.2
• 学会代码：KZLL
• 会议名称：第36届中国控制会议
• 会议地点：中国辽宁大连
• 主办单位：中国自动化学会控制理论专业委员会
• 学会名称：中国自动化学会控制理论专业委员会
• 页数：6
• 文件大小：502k
• 原文格式：D
• 会议级别：全国

摘要

This paper investigates a low-complexity prescribed performance control approach for combined spacecraft with an unknown captured object in the presence of external disturbance. First, a prescribed performance function with appropriate parameters is selected for the filtered state variables involving the attitude and angular velocity. Then, a low-complexity robust prescribed performance controller is developed without any priori knowledge of the inertial information of combined spacecraft.This dramatically decreases the complexity of controller design for combined spacecraft with large uncertainty owing to the fact that the tedious identification of inertial property is avoided. Finally, an illustrative example is employed to validate the effectiveness of proposed control approach in terms of stabilizing the combined spacecraft.
This paper investigates a low-complexity prescribed performance control approach for combined spacecraft with an unknown captured object in the presence of external disturbance. First, a prescribed performance function with appropriate parameters is selected for the filtered state variables involving the attitude and angular velocity. Then, a low-complexity robust prescribed performance controller is developed without any priori knowledge of the inertial information of combined spacecraft.This dramatically decreases the complexity of controller design for combined spacecraft with large uncertainty owing to the fact that the tedious identification of inertial property is avoided. Finally, an illustrative example is employed to validate the effectiveness of proposed control approach in terms of stabilizing the combined spacecraft.

引文

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