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Review of trajectory design and optimization methods for ice giant exploration

Guoliang Liang Yu Zhang Hongwei Yang Hexi Baoyin

航天动力学（英文）2026，Vol.10Issue(2)：199-218,20.

航天动力学（英文）2026，Vol.10Issue(2)：199-218,20.DOI:10.1007/s42064-026-0308-6

Review of trajectory design and optimization methods for ice giant exploration

Guoliang Liang ¹Yu Zhang ¹Hongwei Yang ¹Hexi Baoyin²

作者信息

1. College of Astronautics,Nanjing University of Aeronautics and Astronautics,Nanjing 211106,China
2. School of Aerospace Engineering,Tsinghua University,Beijing 100084,China
折叠

摘要

关键词

ice giant system exploration/Uranus/Neptune/trajectory design and optimization/space missions/aerospace dynamics and control

Key words

ice giant system exploration/Uranus/Neptune/trajectory design and optimization/space missions/aerospace dynamics and control

引用本文复制引用

Guoliang Liang,Yu Zhang,Hongwei Yang,Hexi Baoyin..Review of trajectory design and optimization methods for ice giant exploration[J].航天动力学（英文）,2026,10(2):199-218,20.

基金项目

This work was supported by the National Natural Science Foundation of China(No.12372046),the Natural Science Foundation of Jiangsu Province(No.BK20220130),and the Fundamental Research Funds for the Central Universities(No.NE2025008). （No.12372046）

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