摘要
An approach to basic trajectory design, which allows extension of the classical two-impulse transfer strategy by using the planetary swingby techniques was studied. This approach can effectively reduce the launch energy and the total velocity increments, thereby including a large number of potentially accessible targets. This work presents a significant reference for mission designer when selecting the scientifically significant and technically feasible target for a space mission.
源语言 | 英语 |
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页(从-至) | 502-505 |
页数 | 4 |
期刊 | Journal of Guidance, Control, and Dynamics |
卷 | 29 |
期 | 2 |
DOI | |
出版状态 | 已出版 - 2006 |
已对外发布 | 是 |