An integrated solution to ACMM problem of spacecraft with inertia uncertainty

doi:10.1002/rnc.4332

CSpace > 系统科学研究所

	An integrated solution to ACMM problem of spacecraft with inertia uncertainty
	Liu, Ping 1; Xue, Wenchao2 ; Chen, Sen 2; Huang, Yi2 ; Sun, Zhendong2
	2018-11-25
发表期刊	INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL
ISSN	1049-8923
卷号	28 期号:17 页码:5575-5589
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.
关键词	attitude control and momentum management extended state observer nonlinear control velocity-free spacecraft uncertainty attenuation
DOI	10.1002/rnc.4332
语种	英语
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
WOS类目	Automation & Control Systems ; Engineering, Electrical & Electronic ; Mathematics, Applied
WOS记录号	WOS:000449553000024
出版者	WILEY
引用统计
文献类型	期刊论文
条目标识符	http://ir.amss.ac.cn/handle/2S8OKBNM/31710
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.