An online generation method of ascent trajectory based on feedforward neural networks-Reference-Cited by-同舟云学术

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An online generation method of ascent trajectory based on feedforward neural networks

Published:2022-09 Issue: Volume:128 Page:107739
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Xin,Dai Pei^ORCID,Cheng Xiaoming,Liu Yunzhao,Cui Jiashan^ORCID,Zhang Lihua,Feng Dongzhu

Funder

National Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

Shanxi Provincial Key Research and Development Project

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference48 articles.

1. The Space Shuttle ascent guidance and control;Schleich,1982

2. Space Shuttle ascent guidance, navigation, and control;McHenry;J. Astronaut. Sci.,1979

3. Closed-loop endoatmospheric ascent guidance;Lu;J. Guid. Control Dyn.,2003

4. Ascent guidance for responsive launch: a fixed-point approach;Lu,2005

5. A review of optimization techniques in spacecraft flight trajectory design;Chai;Prog. Aerosp. Sci.,2019

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