Attitude and Orbit Optimal Control of Combined Spacecraft via a Fully-Actuated System Approach
查看参考文献41篇
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文摘
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This paper investigates the attitude and orbit control for the combined spacecraft formed after a target spacecraft without the autonomous control ability is captured by a service spacecraft. The optimal controller of fully-actuated system is proposed to realize the attitude and orbit stabilization control of combined spacecraft. The stability of the system is proved by introducing Lyapunov function. Numerical simulation of the combined spacecraft and physical experiment based on the combined spacecraft simulator (CSS) are completed. Both simulation and experiment results demonstrate the effectiveness and practicability of the optimal controller of fully-actuated system. |
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来源
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Journal of Systems Science and Complexity
,2022,35(2):623-640 【核心库】
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DOI
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10.1007/s11424-022-1492-y
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关键词
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Attitude control
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combined spacecraft
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fully-actuated system
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optimal controller
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orbit control
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地址
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1.
Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin, 150001
2.
Department of Electronic and Electrical Engineering, Southern University of Science and Technology, Shenzhen, 518055
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语种
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英文 |
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文献类型
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研究性论文 |
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ISSN
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1009-6124 |
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学科
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自动化技术、计算机技术;航天(宇宙航行) |
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基金
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国家自然科学基金
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文献收藏号
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CSCD:7238864
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参考文献 共
41
共3页
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