Knowledge Management System of Institue of Mechanics, CAS
| 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)
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| Source Publication | Chinese Space Science and Technology
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| 2002 | |
| Issue | 2Pages: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. |
| Files in This Item: | Download All | |||||
| File Name/Size | DocType | Version | Access | License | ||
| 航天器相对运动与Hill解的适用性分析.（245KB） | 开放获取 | -- | View Download | |||
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