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Combined trajectory and time-planning strategy for rendezvous missions using low-thrust transfer

Jia Guo Zhaojun Pang Zhonghua Du

航天动力学（英文）2025，Vol.9Issue(4)：481-493,13.

航天动力学（英文）2025，Vol.9Issue(4)：481-493,13.DOI:10.1007/s42064-024-0222-8

Combined trajectory and time-planning strategy for rendezvous missions using low-thrust transfer

Jia Guo ¹Zhaojun Pang ¹Zhonghua Du¹

作者信息

1. School of Mechanical Engineering,Nanjing University of Science and Technology,Nanjing 210094,China
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摘要

关键词

low-thrust transfer/orbit optimization/shape-based method/space debris

Key words

low-thrust transfer/orbit optimization/shape-based method/space debris

引用本文复制引用

Jia Guo,Zhaojun Pang,Zhonghua Du..Combined trajectory and time-planning strategy for rendezvous missions using low-thrust transfer[J].航天动力学（英文）,2025,9(4):481-493,13.

基金项目

This work was supported in part by Science and Technology on Space Intelligent Control Laboratory Grants(HTKJ2021KL502010)and the Research Project of Space Debris and Near-Earth Asteroid Defense(KJSP2020010303). （HTKJ2021KL502010）

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