Low-energy transfers to the Moon with long transfer time

Kenta Oshima*, Francesco Topputo, Tomohiro Yanao

*この研究の対応する著者

研究成果: Article査読

16 被引用数 (Scopus)

抄録

This paper globally explores two-impulse, low-energy Earth–Moon transfers in the planar bicircular restricted four-body problem with transfer time of up to 200 days. A grid search combined with a direct transcription and multiple shooting technique reveals numerous families of optimal low-energy solutions, including some that have not been reported yet. We investigate characteristics of solutions in terms of parameters in two- and three-body dynamics, and discuss a trade-off between cost and transfer time based on Pareto-optimal solutions, with and without lunar gravity assists. Analysis of orbital characteristics reveals the role of the Sun, the Earth, and the Moon in the transfer dynamics.

本文言語English
論文番号4
ジャーナルCelestial Mechanics and Dynamical Astronomy
131
1
DOI
出版ステータスPublished - 2019 1月 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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