Global search for low-thrust transfers to the moon in the planar circular restricted three-body problem

Kenta Oshima, Stefano Campagnola, Tomohiro Yanao

研究成果: Conference contribution

1 被引用数 (Scopus)

抄録

The present study globally searches for low-thrust transfers to the Moon in the planar, circular, restricted, three-body problem. To reduce the dimensionality of parameters for determining initial costates, we narrow down candidates of solutions to those satisfying the necessary conditions for optimality based on the indirect method and use an analogy with the two-body dynamics for the initial periodic orbit around the Earth. We obtain a wide range of Pareto solutions in terms of time of flight and mass consumption. Several solutions exploit resonant lunar gravity assists to reduce fuel consumption.

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415-433
ページ数19
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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