首页|期刊导航|航天动力学（英文）|Descent-trajectory planning of a multi-node flexible small celestial body lander in hazardous terrains

Descent-trajectory planning of a multi-node flexible small celestial body lander in hazardous terrains

Jingxuan Chai Youmin Gong Jie Mei Guangfu Ma Weiren Wu

航天动力学（英文）2025，Vol.9Issue(4)：605-619,15.

航天动力学（英文）2025，Vol.9Issue(4)：605-619,15.DOI:10.1007/s42064-024-0244-2

Descent-trajectory planning of a multi-node flexible small celestial body lander in hazardous terrains

Jingxuan Chai ¹Youmin Gong ²Jie Mei ²Guangfu Ma ²Weiren Wu¹

作者信息

1. Institute of Space Science and Applied Technology,Harbin Institute of Technology(Shenzhen),Shenzhen,China
2. School of Mechanical Engineering and Automation,Harbin Institute of Technology(Shenzhen),Shenzhen,China
折叠

摘要

关键词

small celestial body landing/vector field/flow field/trajectory planning/multi-node flexible lander

Key words

small celestial body landing/vector field/flow field/trajectory planning/multi-node flexible lander

引用本文复制引用

Jingxuan Chai,Youmin Gong,Jie Mei,Guangfu Ma,Weiren Wu..Descent-trajectory planning of a multi-node flexible small celestial body lander in hazardous terrains[J].航天动力学（英文）,2025,9(4):605-619,15.

基金项目

This work was supported by the National Key R&D Program(grant number 2019YFA0706500)and the National Defense Basic Research Projects(grant number JCKY2021603B030). （grant number 2019YFA0706500）

航天动力学（英文）

访问量0

下载量0

段落导航