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Trajectory design for awaiting comets on invariant manifolds with optimal control

Soi Yamaguchi Naoki Hiraiwa Mai Bando Shinji Hokamoto Damennick B.Henry Daniel J.Scheeres

航天动力学（英文）2025，Vol.9Issue(4)：565-581,17.

航天动力学（英文）2025，Vol.9Issue(4)：565-581,17.DOI:10.1007/s42064-024-0236-2

Trajectory design for awaiting comets on invariant manifolds with optimal control

Soi Yamaguchi ¹Naoki Hiraiwa ¹Mai Bando ¹Shinji Hokamoto ¹Damennick B.Henry ²Daniel J.Scheeres²

作者信息

1. Department of Aeronautics and Astronautics,Kyushu University,Fukuoka 819-0395,Japan
2. Department of Aerospace Engineering Sciences,University of Colorado Boulder,Boulder 80303,USA
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摘要

关键词

CRTBP/low-thrust/invariant tori/optimal control/spacecraft formation flying

Key words

CRTBP/low-thrust/invariant tori/optimal control/spacecraft formation flying

引用本文复制引用

Soi Yamaguchi,Naoki Hiraiwa,Mai Bando,Shinji Hokamoto,Damennick B.Henry,Daniel J.Scheeres..Trajectory design for awaiting comets on invariant manifolds with optimal control[J].航天动力学（英文）,2025,9(4):565-581,17.

基金项目

The work of the second author was supported by JSPS KAKENHI(Grant Number JP 23KJ1692).The work of the third author was partially supported by Japan Science and Technology Agency,Fusion Oriented Research for Disruptive Science and Technology(JST FOREST Program)(Grant Number JPMJFR206M),and Grant-in-Aid for Scientific Research from the Japan Society for the Promotion of Science(Grant Number 22H03663). （Grant Number JP 23KJ1692）

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