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	Adaptive surrogate model-based fast path planning for spacecraft formation reconfiguration on libration point orbits
	Peng, Haijun; Wang, Wei
刊名	AEROSPACE SCIENCE AND TECHNOLOGY
	2016
卷号	54页码:151-163
关键词	Spacecraft formation reconfiguration Fast path planning Adaptive surrogate model Libration point orbit Circular restricted three-body problem
ISSN号	1270-9638
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/4368701
专题	大连理工大学
作者单位	1.Dalian Univ Technol, Dept Engn Mech, State Key Lab Struct Anal Ind Equipment, Dalian 116024, Peoples R China. 2.Tsinghua Univ, Dept Engn Mech, Beijing 100084, Peoples R China.
推荐引用方式 GB/T 7714	Peng, Haijun,Wang, Wei. Adaptive surrogate model-based fast path planning for spacecraft formation reconfiguration on libration point orbits[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2016,54:151-163.
APA	Peng, Haijun,&Wang, Wei.(2016).Adaptive surrogate model-based fast path planning for spacecraft formation reconfiguration on libration point orbits.AEROSPACE SCIENCE AND TECHNOLOGY,54,151-163.
MLA	Peng, Haijun,et al."Adaptive surrogate model-based fast path planning for spacecraft formation reconfiguration on libration point orbits".AEROSPACE SCIENCE AND TECHNOLOGY 54(2016):151-163.

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