Hybrid Diagnosis System for Aeroengine Sensor and Actuator Faults-Reference-Cited by-同舟云学术

Hybrid Diagnosis System for Aeroengine Sensor and Actuator Faults

Published:2020-01 Issue:1 Volume:33 Page:04019108
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Yuan Ye¹,Ding Shuiting²,Liu Xiaofeng³^ORCID,Pan Qiang⁴^ORCID

Affiliation:

1. Ph.D. Candidate, School of Energy and Power Engineering, Beihang Univ., No. 37 Xueyuan Rd., Haidian District, Beijing 100191, China.

2. Professor, School of Energy and Power Engineering, Beihang Univ., No. 37 Xueyuan Rd., Haidian District, Beijing 100191, China.

3. Associate Professor, School of Transportation Science and Engineering, Beihang Univ., No. 37 Xueyuan Rd., Haidian District, Beijing 100191, China. ORCID: .

4. Lecturer, School of Transportation Science and Engineering, Beihang Univ., No. 37 Xueyuan Rd., Haidian District, Beijing 100191, China (corresponding author). ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001105

Reference27 articles.

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2. Behbahani A. S. Adibhatla and C. Rauche. 2009. “Integrated model-based controls and PHM for improving turbine engine performance reliability and cost.” In Proc. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conf. and Exhibit. Reston VA: American Institute of Aeronautics and Astronautics.

3. Online fault-tolerant onboard aeroengine model tuning structure;Ding S.;Int. J. Aerosp. Eng.,2016

4. An Onboard Aeroengine Model-Tuning System

5. Observer-based fault-tolerant control for an air-breathing hypersonic vehicle model

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