首页|期刊导航|航天动力学（英文）|Bounds of relative motion for resonant solar-sail halo orbits in Earth-Moon system

Bounds of relative motion for resonant solar-sail halo orbits in Earth-Moon system

Chen Gao Kai Zhang Zichen Deng Wei Wang

航天动力学（英文）2025，Vol.9Issue(5)：807-820,14.

航天动力学（英文）2025，Vol.9Issue(5)：807-820,14.DOI:10.1007/s42064-024-0258-9

Bounds of relative motion for resonant solar-sail halo orbits in Earth-Moon system

Chen Gao ¹Kai Zhang ¹Zichen Deng ¹Wei Wang²

作者信息

1. School of Mechanics and Transportation Engineering,MIIT Key Laboratory of Dynamics and Control of Complex Systems,Northwestern Polytechnical University,Xi'an 710072,China
2. School of Aeronautics and Astronautics,Shanghai Jiao Tong University,Shanghai,China
折叠

摘要

关键词

relative motion/jet transport technique/solar sail/Earth-Moon system

Key words

relative motion/jet transport technique/solar sail/Earth-Moon system

引用本文复制引用

Chen Gao,Kai Zhang,Zichen Deng,Wei Wang..Bounds of relative motion for resonant solar-sail halo orbits in Earth-Moon system[J].航天动力学（英文）,2025,9(5):807-820,14.

基金项目

This study was supported by the National Key R&D Program of China(Grant No.2022YFC2204800)and the Fundamental Research Funds for the Central Universities(Grant No.D5000240142),the National Natural Science Foundation of China(Grant No.12272223),the Natural Science Foundation of Shanghai(Grant No.23ZR1433600),and the State Key Laboratory of Mechanics and Control for Aerospace Structures(Grant No.MCMS-E-0223G01). （Grant No.2022YFC2204800）

航天动力学（英文）

访问量0

下载量0

段落导航