Research on Over-Speed Protection Control Method for Aircraft Engines Based on Control Barrier Functions-Reference-Cited by-同舟云学术

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Research on Over-Speed Protection Control Method for Aircraft Engines Based on Control Barrier Functions

Published:2024-03-01 Issue: Volume:42 Page:1233-1237
ISSN:
Container-title:2024 7th International Conference on Advanced Algorithms and Control Engineering (ICAACE)
language:
Short-container-title:

Author:

Jie Bai¹,Xu Zeliang¹

Affiliation:

1. Civil Aviation University of China,Key Laboratory of Civil Aircraft Airworthiness Technology,Tianjin,China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx8/10548022/10548040/10549283.pdf?arnumber=10549283

Reference14 articles.

1. Aircraft Engine Controls

2. Turbofan engine limit protection closed-loop control design [J];Xi;Aeroengine,2016

3. Aeroengine Restriction Management Control Method Research [D];Jiakun;Nanjing University of Aeronautics and Astronautics,2023

4. Optimization design of turbofan engine limit protection controller based on condition judgment criterion [J];Jie;Aeroengine,2022

5. Restricted protection control method for turbofan engine based on improved model-free adaptive algorithm [J];Tingyun;Propulsion technology,2020

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