Design of lunar landing trajectory under constraints

	Design of lunar landing trajectory under constraints
	Huang, C; Hu, XG ; Li, X
刊名	CHINESE ASTRONOMY AND ASTROPHYSICS
	2001-10-01
卷号	25 期号:4 页码:464-477
关键词	lunar landing orbit design constraint
英文摘要	The design of a lunar landing trajectory which satisfies certain constraints is considered and discussed. The constraints are of two kinds, kinetic constraints, which deal with the relative positions among the Sun, the Moon, the Earth, the spacecraft and tracking stations, and dynamic constraints, which deal with the orbital motion of the spacecraft. After a discussion of the characteristics of lunar flight trajectory, a method of designing standard flight trajectory is suggested that satisfies the constraints. This method is applied to the Chinese lunar landing flight and to the pre-design of the orbit of a lunar satellite.
WOS标题词	Science & Technology ; Physical Sciences
类目[WOS]	Astronomy & Astrophysics
研究领域[WOS]	Astronomy & Astrophysics
收录类别	SCI
语种	英语
WOS记录号	WOS:000172661300010
公开日期	2010-07-30
内容类型	期刊论文
源URL	[http://119.78.226.72//handle/331011/10934]
专题	上海天文台_天文地球动力学研究中心
作者单位	1.Acad Sinica, Shanghai Observ, Shanghai 200030, Peoples R China 2.Chinese Acad Sci, Natl Astron Observ, Beijing 100012, Peoples R China
推荐引用方式 GB/T 7714	Huang, C,Hu, XG,Li, X. Design of lunar landing trajectory under constraints[J]. CHINESE ASTRONOMY AND ASTROPHYSICS,2001,25(4):464-477.
APA	Huang, C,Hu, XG,&Li, X.(2001).Design of lunar landing trajectory under constraints.CHINESE ASTRONOMY AND ASTROPHYSICS,25(4),464-477.
MLA	Huang, C,et al."Design of lunar landing trajectory under constraints".CHINESE ASTRONOMY AND ASTROPHYSICS 25.4(2001):464-477.