Abstract
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.
Original language | English |
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Pages (from-to) | 1136-1145 |
Number of pages | 10 |
Journal | Journal of Guidance, Control, and Dynamics |
Volume | 42 |
Issue number | 5 |
DOIs | |
Publication status | Published - 2019 |