Surrogate-based entire trajectory optimization for full space mission from launch to reentry-Reference-Cited by-同舟云学术

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Surrogate-based entire trajectory optimization for full space mission from launch to reentry

Published:2022-01 Issue: Volume:190 Page:83-97
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

He Xingji^ORCID,Zuo Xiaoyu^ORCID,Li Qinglong^ORCID,Xu Ming^ORCID,Li Jian

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference41 articles.

1. X-37B orbital test vehicle and derivatives;Grantz,2011

2. History of space shuttle rendezvous and proximity operations;Goodman;J. Spacecraft Rockets,2006

3. Approach for on-orbit maintenance and experiment plan using 150kg-class satellites;Kimura,2005

4. DLR reusability flight experiment ReFEx;Bauer;Acta Astronaut.,2020

5. Trajectory planning for hypersonic reentry vehicle satisfying deterministic and probabilistic constraints;Chai;Acta Astronaut.,2020

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. An Improved PSO Algorithm for Hypersonic Vehicle Cruise Trajectory Planning;Lecture Notes in Electrical Engineering;2024

2. Adaptive Surrogate-Assisted Optimal Sailboat Path Search Using Onboard Computers;Computational Science – ICCS 2022;2022

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