An integrated solution to ACMM problem of spacecraft with inertia uncertainty-Reference-Cited by-同舟云学术

An integrated solution to ACMM problem of spacecraft with inertia uncertainty

Published:2018-09-19 Issue:17 Volume:28 Page:5575-5589
ISSN:1049-8923
Container-title:International Journal of Robust and Nonlinear Control
language:en
Short-container-title:Int J Robust Nonlinear Control

Author:

Liu Ping¹^ORCID,Xue Wenchao²^ORCID,Chen Sen²,Huang Yi²,Sun Zhendong²^ORCID

Affiliation:

1. School of Electrical Engineering and Intelligentization; Dongguan University of Technology; Dongguan China

2. Key Laboratory of Systems and Control; Academy of Mathematics and Systems Science, Chinese Academy of Sciences; Beijing China

Funder

Ministry of Science and Technology of the People's Republic of China

National Natural Science Foundation of China

Publisher

Wiley

Subject

Electrical and Electronic Engineering,Industrial and Manufacturing Engineering,Mechanical Engineering,Aerospace Engineering,Biomedical Engineering,General Chemical Engineering,Control and Systems Engineering

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1002/rnc.4332/fullpdf

Reference35 articles.

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4. Multistage design of an optimal momentum management controller for the Space Station;Sunkel;J Guid Control Dyn,1991

5. Innovative approach to the momentum management control for Space Station freedom;Mapar;J Guid Control Dyn,1993

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