Optimization Method for Launch Vehicle Attitude Control Parameters Based on Bayesian Optimization-Reference-Cited by-同舟云学术

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Optimization Method for Launch Vehicle Attitude Control Parameters Based on Bayesian Optimization

Published:2024-05-25 Issue: Volume:1, 2, 3 Page:4164-4169
ISSN:
Container-title:2024 36th Chinese Control and Decision Conference (CCDC)
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Author:

Tianpeng Lan¹,Jiarun Liu¹,Yue Peng²,Xu Huang¹,Yu Zhao¹

Affiliation:

1. Beijing Aerospace Automatic Control Institute,National Key Laboratory of Science and Technology on Aerospace Intelligence Control,Beijing,China

2. Beijing Aerospace Automatic Control Institute,National Key Laboratory of Science and Technology on Aerospace Intelligence Control,Beijing,China,157243

Funder

Nature

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx8/10587298/10587321/10588209.pdf?arnumber=10588209

Reference10 articles.

1. Automatic Design Technology of Control Laws for Launch Vehicles Based on Genetic Algorithm;Minfeng,2007

2. Constrained Bayesian Optimization with Noisy Experiments

3. Recent Advances in Bayesian Optimization

4. Survey on Bayesian Optimization Methodology and Applications;Jiaxu;Journal of Software,2018

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