Strong Robust Attitude Control of the Large Launch Vehicle Based on Backstepping Design Approach-Reference-Cited by-同舟云学术

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Strong Robust Attitude Control of the Large Launch Vehicle Based on Backstepping Design Approach

Published:2024-05-25 Issue: Volume:42 Page:5143-5148
ISSN:
Container-title:2024 36th Chinese Control and Decision Conference (CCDC)
language:
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Author:

Chen Hongbo¹,Zhao Boyan¹,Ma Zhenwei¹,Wang Guanjun¹

Affiliation:

1. Sun Yat-sen University,School of Systems Science and Engineering,Guangzhou,China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx8/10587298/10587321/10588169.pdf?arnumber=10588169

Reference20 articles.

1. ADP-based intelligent attitude fault-tolerant control for launch vehicles;Liang;Acta Aeronautica et Astronautica Sinica,2021

2. Space launch vehicle’s development in China;Lu;Astronautical Systems Enginerring Technology,2017

3. Ballistic trajectory correction algorithms of high-spin rocket based on impact point prediction;Yang;Acta Aeronautica et Astronautica Sinica,2020

4. Global and robust attitude control of a launch vehicle in exoatmospheric flight

5. Current status and development of spacecraft attitude fault-tolerant control technology;Qing;Journal of Telemetry, Tracking and Command,2022

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