Sparse optimal trajectory design in three-body problem

研究成果: Chapter in Book/Report/Conference proceedingConference contribution

1 被引用数 (Scopus)

抄録

A structure of the optimal trajectory for minimizing fuel consumption in an unstable dynamical environment such as the three-body problem is not well studied. Recently, it has been found that a sparse solution structure appears in the optimal control of a dynamical system. The concept of sparsity explains the property that the minimum fuel trajectory corresponds to the trajectory which minimizes the total thrusting time. In this paper, we propose a numerical method to obtain the minimum fuel sparse optimal trajectory in the unstable dynamical system. As an example, proposed methods are applied to the transfer in the Sun-Earth system.

本文言語英語
ホスト出版物のタイトルSpaceflight Mechanics 2019
編集者Francesco Topputo, Andrew J. Sinclair, Matthew P. Wilkins, Renato Zanetti
出版社Univelt Inc.
ページ2599-2618
ページ数20
ISBN(印刷版)9780877036593
出版ステータス出版済み - 1 1 2019
イベント29th AAS/AIAA Space Flight Mechanics Meeting, 2019 - Maui, 米国
継続期間: 1 13 20191 17 2019

出版物シリーズ

名前Advances in the Astronautical Sciences
168
ISSN(印刷版)0065-3438

会議

会議29th AAS/AIAA Space Flight Mechanics Meeting, 2019
国/地域米国
CityMaui
Period1/13/191/17/19

All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • 宇宙惑星科学

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