摘要
Energy-saving capture at mars via backward-stable orbits is investigated in a study. The study focuses on exploiting the backward-stable orbits, such as -1-stable orbits for powered capture at Mars. The capture occurs at the lowest periareion of the backward-stable orbits and transits the spacecraft from the interplanetary trajectory to the capture trajectory. It is demonstrated that the periapsis states of the backward-stable orbits with respect to Mars will change in each circle, which might provide a better periareion state than the initial state to reduce the capture cost, and that apture happens within the sphere of influence (SOI) of Mars.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 1136-1145 |
| 页数 | 10 |
| 期刊 | Journal of Guidance, Control, and Dynamics |
| 卷 | 42 |
| 期 | 5 |
| DOI | |
| 出版状态 | 已出版 - 2019 |
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