An integrated solution to ACMM problem of spacecraft with inertia uncertainty
文献类型：期刊论文
| 作者 | Liu, Ping1; Xue, Wenchao2 ; Chen, Sen2; Huang, Yi2; Sun, Zhendong2
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| 刊名 | INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL
 |
| 出版日期 | 2018-11-25 |
| 卷号 | 28期号:17页码:5575-5589 |
| 关键词 | attitude control and momentum management extended state observer nonlinear control velocity-free spacecraft uncertainty attenuation |
| ISSN号 | 1049-8923 |
| DOI | 10.1002/rnc.4332 |
| 英文摘要 | In this work, an integrated solution to the attitude control and momentum management problem is studied for the velocity-free large spacecraft subject to both inertia uncertainty and strong disturbances. A multiple-input-multiple-output-type linear extended state observer is constructed to estimate the uncertain information, and a novel disturbance compensator and a linear quadratic regulator controller are proposed. The stability of the proposed scheme is rigorously proved, and the quantitative relationship between the closed-loop tracking error and the uncertainty size is thoroughly analyzed. Comparison studies are carried out to verify the effectiveness and robustness of the proposed approach. |
| 资助项目 | National Key Basic Research Program of China[2014CB845302] ; National Natural Science Foundation of China[61603380] ; National Natural Science Foundation of China[61633003-3] |
| WOS研究方向 | Automation & Control Systems ; Engineering ; Mathematics |
| 语种 | 英语 |
| WOS记录号 | WOS:000449553000024 |
| 出版者 | WILEY |
| 源URL | [http://ir.amss.ac.cn/handle/2S8OKBNM/31709]  |
| 专题 | 系统科学研究所 |
| 通讯作者 | Sun, Zhendong |
| 作者单位 | 1.Dongguan Univ Technol, Sch Elect Engn & Intelligentizat, Dongguan, Peoples R China 2.Chinese Acad Sci, Acad Math & Syst Sci, Key Lab Syst & Control, Beijing 100190, Peoples R China |
| 推荐引用方式 GB/T 7714 | Liu, Ping,Xue, Wenchao,Chen, Sen,et al. An integrated solution to ACMM problem of spacecraft with inertia uncertainty[J]. INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL,2018,28(17):5575-5589. |
| APA | Liu, Ping,Xue, Wenchao,Chen, Sen,Huang, Yi,&Sun, Zhendong.(2018).An integrated solution to ACMM problem of spacecraft with inertia uncertainty.INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL,28(17),5575-5589. |
| MLA | Liu, Ping,et al."An integrated solution to ACMM problem of spacecraft with inertia uncertainty".INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL 28.17(2018):5575-5589. |
入库方式： OAI收割
来源：数学与系统科学研究院
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