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	Cluster flight control for fractionated spacecraft on an elliptic orbit
	Xu, Ming; Liang, Yuying; Tan, Tian; Wei, Lixin
刊名	CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY
	2016
卷号	125页码:383-412
关键词	Hamiltonian structure-preserving control Cluster flight Bounded and quasi-periodic relative trajectories Elliptic orbit Floquet stability
ISSN号	0923-2958
DOI	10.1007/s10569-016-9685-0
URL标识	查看原文
收录类别	SCIE
WOS记录号	WOS:000379624700001
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5954016
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Xu, Ming,Liang, Yuying,Tan, Tian,et al. Cluster flight control for fractionated spacecraft on an elliptic orbit[J]. CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY,2016,125:383-412.
APA	Xu, Ming,Liang, Yuying,Tan, Tian,&Wei, Lixin.(2016).Cluster flight control for fractionated spacecraft on an elliptic orbit.CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY,125,383-412.
MLA	Xu, Ming,et al."Cluster flight control for fractionated spacecraft on an elliptic orbit".CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY 125(2016):383-412.

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