Sparse optimal trajectory design in three-body problem

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

抜粋

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.

元の言語英語
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
出版者Univelt Inc.
ページ2599-2618
ページ数20
ISBN(印刷物)9780877036593
出版物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(印刷物)0065-3438

会議

会議29th AAS/AIAA Space Flight Mechanics Meeting, 2019
米国
Maui
期間1/13/191/17/19

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

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  • これを引用

    Kayama, Y., Bando, M., & Hokamoto, S. (2019). Sparse optimal trajectory design in three-body problem. : F. Topputo, A. J. Sinclair, M. P. Wilkins, & R. Zanetti (版), Spaceflight Mechanics 2019 (pp. 2599-2618). [AAS 19-359] (Advances in the Astronautical Sciences; 巻数 168). Univelt Inc..