Analysis of Spacecraft Relative Motion and Applicability of Hill's Solution

IMECH-IR > 力学所知识产出(1956-2008)

	Analysis of Spacecraft Relative Motion and Applicability of Hill's Solution
	Zhang ZM(张振民); Xu B(许滨); Zhang H(张珩); Sun L(孙兰); Pan LJ(潘力均)
Source Publication	Chinese Space Science and Technology
	2002
Issue	2 Pages:1-8
ISSN	1000-758X
Other Abstract	研究了空间飞行器编队中最具基础性的问题之一,即相对运动的解析表达及Hill方程的适用条件。通过建立相对运动的通解公式,针对不同性质的初值深入地分析了其相对运动轨迹的本质特征,并给出了Hill方程的适用条件。此外,文中还给出了一个新的编队设计简化公式。
Subject Area	力学
Indexed By	其他
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/17477
Collection	力学所知识产出(1956-2008)
Recommended Citation GB/T 7714	Zhang ZM,Xu B,Zhang H,et al. Analysis of Spacecraft Relative Motion and Applicability of Hill's Solution[J]. Chinese Space Science and Technology,2002,2,:1-8.
APA	张振民,许滨,张珩,孙兰,&潘力均.(2002).Analysis of Spacecraft Relative Motion and Applicability of Hill's Solution.Chinese Space Science and Technology(2),1-8.
MLA	张振民,et al."Analysis of Spacecraft Relative Motion and Applicability of Hill's Solution".Chinese Space Science and Technology .2(2002):1-8.

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