Trajectory design to mars from earth-moon system with three-dimensional transit orbits

Wataru Noma, Zhe Xu, Mai Bando, Shinji Hokamoto

研究成果: Contribution to journalConference article査読

抄録

In planetary exploration, designing low-energy trajectories is important to reduce the fuel. This study focuses on the trajectory design which reduces the total ?v using three-dimensional transit orbits. There are two benefits of using transit orbits: the first one is that the design is easier than connecting manifolds of different three-body system, and the other is that a trajectory suitable for transfer to Mars can be selected by considering transit orbits with various Jacobi constant. Thus, three-dimensional transit orbits can significantly increase the freedom of trajectory design. Therefore this paper presents the three-dimensional transit orbit family with various Jacobi constant. As an application, a trajectory optimization from Moon L2 point periodic orbit to Mars is shown.

本文言語英語
ジャーナルProceedings of the International Astronautical Congress, IAC
2020-October
出版ステータス出版済み - 2020
イベント71st International Astronautical Congress, IAC 2020 - Virtual, Online
継続期間: 10 12 202010 14 2020

All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • 天文学と天体物理学
  • 宇宙惑星科学

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