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	Optimal control of attitude for coupled-rigid-body spacecraft via Chebyshev-Gauss pseudospectral method
	Ge, Xinsheng[1]; Yi, Zhonggui[2]; Chen, Liqun[3]
刊名	APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION
	2017
卷号	38页码:1257-1272
关键词	coupled rigid body spacecraft optimal control pseudospectral method (PM) Chebyshev-Gauss (CG) point
ISSN号	0253-4827
URL标识	查看原文
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/2185337
专题	上海大学
作者单位	1.[1]Beijing Informat Sci & Technol Univ, Coll Sci, Beijing 100192, Peoples R China. 2.[2]Beijing Informat Sci & Technol Univ, Coll Mech & Elect Engn, Beijing 100192, Peoples R China. 3.[3]Shanghai Univ, Shanghai Inst Appl Math & Mech, Shanghai 200072, Peoples R China.
推荐引用方式 GB/T 7714	Ge, Xinsheng[1],Yi, Zhonggui[2],Chen, Liqun[3]. Optimal control of attitude for coupled-rigid-body spacecraft via Chebyshev-Gauss pseudospectral method[J]. APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION,2017,38:1257-1272.
APA	Ge, Xinsheng[1],Yi, Zhonggui[2],&Chen, Liqun[3].(2017).Optimal control of attitude for coupled-rigid-body spacecraft via Chebyshev-Gauss pseudospectral method.APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION,38,1257-1272.
MLA	Ge, Xinsheng[1],et al."Optimal control of attitude for coupled-rigid-body spacecraft via Chebyshev-Gauss pseudospectral method".APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION 38(2017):1257-1272.

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