Optimal trajectory design for safety rendezvous based on sparse modeling

Satoshi Nagashima, Mai Bando, Shinji Hokamoto

研究成果: Contribution to journalConference article査読

抄録

In trajectory design of a spacecraft, reducing the fuel consumption is important factor. In order to find the minimum fuel trajectory, this paper considers the L1 norm as the performance index. This paper discuss design parameters characterizing the L1 optimal trajectory, such as sampling time, flight time and magnitude of thrust. Also, this paper compare with the conventional method from the viewpoint of fuel consumption. In addition, this paper consider the rendezvous problem considering safety.

本文言語英語
ジャーナルProceedings of the International Astronautical Congress, IAC
2018-October
出版ステータス出版済み - 2018
イベント69th International Astronautical Congress: #InvolvingEveryone, IAC 2018 - Bremen, ドイツ
継続期間: 10 1 201810 5 2018

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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