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

Kenta Oshima*, Stefano Campagnola, Tomohiro Yanao

*この研究の対応する著者

研究成果: Article査読

9 被引用数 (Scopus)

抄録

This paper globally searches for low-thrust transfers to the Moon in the planar, circular, restricted, three-body problem. Propellant-mass optimal trajectories are computed with an indirect method, which implements the necessary conditions of optimality based on the Pontryagin principle. We present techniques to reduce the dimension of the set over which the required initial costates are searched. We obtain a wide range of Pareto solutions in terms of time of flight and mass consumption. Using the Tisserand–Poincaré graph, a number of solutions are shown to exploit high-altitude lunar flybys to reduce fuel consumption.

本文言語English
ページ(範囲)303-322
ページ数20
ジャーナルCelestial Mechanics and Dynamical Astronomy
128
2-3
DOI
出版ステータスPublished - 2017 6 1

ASJC Scopus subject areas

  • モデリングとシミュレーション
  • 数理物理学
  • 天文学と天体物理学
  • 宇宙惑星科学
  • 計算数学
  • 応用数学

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