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
Qiao, D., Cui, H., & Cui, P. (2006). Evaluating accessibility of near-earth asteroids via earth gravity assists. Journal of Guidance, Control, and Dynamics, 29(2), 502-505. https://doi.org/10.2514/1.16757