Orbit expressions in the continuous polar coordinate system

Jun Matsumoto, Jun'ichiro Kawaguchi

研究成果: Conference contribution

抄録

This paper shows a new strategy to design low-thrust trajectories by using elaborated rotational coordinates which includes two rotational coordinates used in the circular restricted three-body problems around the departure planet and the target planet. Firstly, a straight-line trajectory in these new coordinates is derived analytically. Secondly, by joining this straight-line trajectory, it can be possible to design low-thrust trajectories which satisfy the boundary conditions easily. In this paper, an example trajectory from Earth to Mars is designed. This example shows the effectiveness of this strategy.

本文言語English
ホスト出版物のタイトルSpace for Our Future - Advances in the Astronautical Sciences
ホスト出版物のサブタイトルProceedings of the 13th International Conference of Pacific-Basin Societies, ISCOPS 2012
ページ85-92
ページ数8
出版ステータスPublished - 2013
外部発表はい
イベント13th International Space Conference of Pacific-Basin Societies, ISCOPS 2012 - Kyoto, Japan
継続期間: 2012 5 152012 5 18

出版物シリーズ

名前Advances in the Astronautical Sciences
146
ISSN(印刷版)0065-3438

Other

Other13th International Space Conference of Pacific-Basin Societies, ISCOPS 2012
国/地域Japan
CityKyoto
Period12/5/1512/5/18

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

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