Predictor-corrector reentry guidance for hypersonic glide vehicles based on high-precision analytical solutions-Reference-Cited by-同舟云学术

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Predictor-corrector reentry guidance for hypersonic glide vehicles based on high-precision analytical solutions

Published:2024-08 Issue: Volume: Page:109545
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Liu Zhengzhuo,Zheng Guodong,Zhang Bo^ORCID,Wei Jianli,Huang Hanqiao,Yan Jie

Publisher

Elsevier BV

Reference37 articles.

1. Entry trajectory planning with terminal full states constraints and multiple geographic constraints;Wang;Aerosp. Sci. Technol.,2019

2. Review of control and guidance technology on hypersonic vehicle;Ding;Chin. J. Aeronaut.,2022

3. Tianwen-1 Mars entry vehicle trajectory and atmosphere reconstruction preliminary analysis;Wei;Astrodynamics,2022

4. Entry guidance with terminal time control based on quasi-equilibrium glide condition;Guo;IEEE Trans. Aerosp. Electron. Syst.,2013

5. Integrated method of guidance, control and morphing for hypersonic morphing vehicle in glide phase;Bao;Chin. J. Aeronaut.,2021

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