Optimal trajectory design for safety rendezvous based on sparse modeling

Satoshi Nagashima, Mai Bando, Shinji Hokamoto

研究成果: ジャーナルへの寄稿Conference article

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 L 1 norm as the performance index. This paper discuss design parameters characterizing the L 1 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.

元の言語英語
ジャーナルProceedings of the International Astronautical Congress, IAC
2018-October
出版物ステータス出版済み - 1 1 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

Fingerprint

rendezvous
safety
fuel consumption
trajectory
Trajectories
trajectories
Fuel consumption
modeling
flight time
norms
thrust
Spacecraft
spacecraft
sampling
flight
Sampling

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Astronomy and Astrophysics
  • Space and Planetary Science

これを引用

Optimal trajectory design for safety rendezvous based on sparse modeling. / Nagashima, Satoshi; Bando, Mai; Hokamoto, Shinji.

:: Proceedings of the International Astronautical Congress, IAC, 巻 2018-October, 01.01.2018.

研究成果: ジャーナルへの寄稿Conference article

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