Fully Actuated System Approach for 6DOF Spacecraft Control Based on Extended State Observer
查看参考文献28篇
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文摘
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This paper deals with the problem of position and attitude tracking control for a rigid spacecraft. A fully actuated system (FAS) model for the six degree-of-freedom (6DOF) spacecraft motion is derived first from the state-space model by variable elimination. Considering the uncertainties from external disturbance, unknown motion information, and uncertain inertia properties, an extended state observer (ESO) is designed to estimate the total disturbance. Then, a tracking controller based on FAS approach is designed, and this makes the closed-loop system a constant linear one with an arbitrarily assignable eigenstructure. The solution to the parameter matrices of the observer and controller is given subsequently. It is proved via the Lyapunov stability theory that the observer errors and tracking errors both converge into the neighborhood of the origin. Finally, numerical simulation demonstrates the effectiveness of the proposed controller. |
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来源
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Journal of Systems Science and Complexity
,2022,35(2):604-622 【核心库】
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DOI
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10.1007/s11424-022-1498-5
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关键词
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Constant linear closed-loop system
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extended state observer
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fully actuated system approach
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relative position and attitude control
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地址
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1.
Center for Control Science and Technology, Southern University of Science and Technology, Shenzhen, 518055
2.
Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin, 150001
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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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supported by the Science Center Program of the National Natural Science Foundation of China
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国家自然科学基金
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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:7238863
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