CSpace  > 系统科学研究所
An integrated solution to ACMM problem of spacecraft with inertia uncertainty
Liu, Ping1; Xue, Wenchao2; Chen, Sen2; Huang, Yi2; Sun, Zhendong2
2018-11-25
Source PublicationINTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL
ISSN1049-8923
Volume28Issue:17Pages:5575-5589
AbstractIn 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.
Keywordattitude control and momentum management extended state observer nonlinear control velocity-free spacecraft uncertainty attenuation
DOI10.1002/rnc.4332
Language英语
Funding ProjectNational Key Basic Research Program of China[2014CB845302] ; National Natural Science Foundation of China[61603380] ; National Natural Science Foundation of China[61633003-3]
WOS Research AreaAutomation & Control Systems ; Engineering ; Mathematics
WOS SubjectAutomation & Control Systems ; Engineering, Electrical & Electronic ; Mathematics, Applied
WOS IDWOS:000449553000024
PublisherWILEY
Citation statistics
Document Type期刊论文
Identifierhttp://ir.amss.ac.cn/handle/2S8OKBNM/31710
Collection系统科学研究所
Affiliation1.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
Recommended Citation
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.
Files in This Item:
There are no files associated with this item.
Related Services
Recommend this item
Bookmark
Usage statistics
Export to Endnote
Google Scholar
Similar articles in Google Scholar
[Liu, Ping]'s Articles
[Xue, Wenchao]'s Articles
[Chen, Sen]'s Articles
Baidu academic
Similar articles in Baidu academic
[Liu, Ping]'s Articles
[Xue, Wenchao]'s Articles
[Chen, Sen]'s Articles
Bing Scholar
Similar articles in Bing Scholar
[Liu, Ping]'s Articles
[Xue, Wenchao]'s Articles
[Chen, Sen]'s Articles
Terms of Use
No data!
Social Bookmark/Share
All comments (0)
No comment.
 

Items in the repository are protected by copyright, with all rights reserved, unless otherwise indicated.