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Lunar soft landing trajectory optimization methods

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

A mathematical model of optimal lunar soft landing problem is given and several common lunar soft landing trajectory optimization methods based on minimum fuel consumption, including Minimum Principle, Ant Colony Op-timization method, Genetic Algorithm and Gauss Pseudospectral method are summarized. Solving steps of different methods are discussed and compared. All optimization methods can meet the constraint requirements and accuracy requirements of lunar soft landing trajectory optimal problem. Simultaneously, different optimization methods has different advantages in solving the problem.

源语言英语
主期刊名IET Conference Publications
出版商Institution of Engineering and Technology
版本CP656
ISBN(印刷版)9781849199285
DOI
出版状态已出版 - 2014
活动International Conference on Cyberspace Technology, CCT 2014 - Beijing, 中国
期限: 8 11月 201410 11月 2014

出版系列

姓名IET Conference Publications
编号CP656
2014

会议

会议International Conference on Cyberspace Technology, CCT 2014
国家/地区中国
Beijing
时期8/11/1410/11/14

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