Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation
查看参考文献34篇
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文摘
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In this paper, a fully-actuated system approach (FASA) based control method is proposed for rigid spacecraft attitude tracking with actuator saturation. First, a second-order fully-actuated form of spacecraft attitude error model is established by modified Rodrigues parameters (MRPs). The unknown total disturbance caused by inertial uncertainty and external disturbance is estimated by using extended state observer, then an FASA based controller is developed. Further, a control parameterization method is adopted to optimize the parameter matrices of FASA based controller with the actuator saturation. Finally, a numerical example is carried out to validate the effectiveness of the proposed scheme. |
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来源
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Journal of Systems Science and Complexity
,2022,35(2):688-702 【核心库】
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DOI
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10.1007/s11424-022-1515-8
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关键词
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Full-actuated system approach
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modified Rodrigues parameters
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parameter optimization
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spacecraft attitude tracking
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地址
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School of Aeronautics and Astronautics, Sichuan University, Chengdu, 610065
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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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Huiyan Project for Research on Innovation and Application of Space Science and Technology
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文献收藏号
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CSCD:7238868
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34
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