The Earth-Moon low-energy transfer in the 4-body problem

Kaori Onozaki, Hiroaki Yoshimura, Shane D. Ross

研究成果: Conference contribution

1 被引用数 (Scopus)

抄録

A low energy transfer from the Earth to the Moon is proposed in the context of the 4-body Problem. We propose a new model by regarding the Sun-Earth-Moon-Spacecraft (S/C) 4-body system as the coupled system of the Sun-perturbed 3-body system and the Moon-perturbed 3-body system. In particular, we clarify the tube structures of invariant manifolds of the 4-body Problem by investigating the Lagrangian coherent structures of such a coupled 3-body system with perturbations. Lastly, we construct a low-energy transfer trajectory from the Earth to the Moon by patching two trajectories obtained from the perturbed systems at a Poincare section. We develop an optimal trajectory by minimizing the Delta-v at the Poincaré section.

本文言語English
ホスト出版物のタイトルSpaceflight Mechanics 2016
編集者Martin T. Ozimek, Renato Zanetti, Angela L. Bowes, Ryan P. Russell, Martin T. Ozimek
出版社Univelt Inc.
ページ1497-1512
ページ数16
ISBN(印刷版)9780877036333
出版ステータスPublished - 2016
イベント26th AAS/AIAA Space Flight Mechanics Meeting, 2016 - Napa, United States
継続期間: 2016 2 142016 2 18

出版物シリーズ

名前Advances in the Astronautical Sciences
158
ISSN(印刷版)0065-3438

Other

Other26th AAS/AIAA Space Flight Mechanics Meeting, 2016
国/地域United States
CityNapa
Period16/2/1416/2/18

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

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