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Full Length Article | Open Access

SAR performance-based fault diagnosis for electro-hydraulic control system: A novel FDI framework for closed-loop system

Yang ZHANGa, Shaoping WANGb, Jian SHIb( ), Xinyu YANGa, Jiarui ZHANGc, Xi WANGa
School of Energy and Power Engineering, Beihang University, Beijing 100191, China
School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China
Institute for Automatic Control and Complex Systems (AKS), University of Duisburg-Essen, Duisburg 47057, Germany

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Model-based fault diagnosis serves as an efficient and powerful technique in addressing fault detection and isolation (FDI) issues for control systems. However, the standard methods and their modifications still encounter some difficulties in algorithm design and application for complex higher-order systems. To avoid these difficulties, a novel fault diagnosis framework based on multiple performance indicators of closed-loop control system is proposed. Under this framework, a so-called performance residual vector is constructed to measure the differences between the real system and the nominal model in terms of system stability, accuracy, and rapidity (SAR) respectively. The criteria for quantification, normalization of the SAR residuals and the explicit mappings between the thresholds and the required performance are given. FDI can be easily achieved simultaneously by monitoring the normalized residual vector length and direction in the SAR performance residual space. A case study on electro-hydraulic servo control system of turbofan engine is adopted to demonstrate the effectiveness of the proposed method.

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Chinese Journal of Aeronautics
Pages 381-392

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Cite this article:
ZHANG Y, WANG S, SHI J, et al. SAR performance-based fault diagnosis for electro-hydraulic control system: A novel FDI framework for closed-loop system. Chinese Journal of Aeronautics, 2022, 35(10): 381-392. https://doi.org/10.1016/j.cja.2021.06.001

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Received: 23 April 2021
Revised: 10 May 2021
Accepted: 18 May 2021
Published: 24 June 2021
© 2021 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).