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 |
|---|---|
| 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 |
指纹
探究 'Evaluating accessibility of near-earth asteroids via earth gravity assists' 的科研主题。它们共同构成独一无二的指纹。引用此
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