Fault-Tolerant Control Allocation System for The Reaction Control System of Hypersonic Vehicles with Multiple Faults-Reference-Cited by-同舟云学术

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Fault-Tolerant Control Allocation System for The Reaction Control System of Hypersonic Vehicles with Multiple Faults

Published:2022-08-15 Issue: Volume: Page:
ISSN:
Container-title:2022 34th Chinese Control and Decision Conference (CCDC)
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Author:

Zhang Yanxue¹,Song Jia²,Feng Jianlin¹,Liu Xiuming¹,Hua Wei¹

Affiliation:

1. Science and Technology on Space Physics Laboratory,Beijing,100076

2. Beihang University,School of Astronautics,Beijing,China,100191

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10032843/10032844/10033552.pdf?arnumber=10033552

Reference16 articles.

1. X-34 propulsion system design

2. Hypersonic Vehicle Simulation Model: Winged-Cone Configuration;shaughnessy,1990

3. An Improvement of PWPF in Reaction Control System of Hypersonic Vehicle;song;Haikou 15th Chinese Intelligent Systems Conference,2019

4. Modeling and flight attitude control for aerospace vehicle’ s reentry through atmosphere;qian;Journal of PLA University of Science and Technology(Natural Science Edition),2010

5. Attitude takeover control for spacecraft with unknown parameter;huang;Kongzhi yu Juece/Control and Decision,2017

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