Design of lunar landing trajectory under constraints
文献类型：期刊论文
| 作者 | Huang, C ; Hu, XG; Li, X
|
| 刊名 | CHINESE ASTRONOMY AND ASTROPHYSICS
 |
| 出版日期 | 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 |
| 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. |
入库方式： OAI收割
来源：上海天文台
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