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An adaptive hybrid fault-tolerant control system design for aeroengine sensor and actuator faults

Published: 25 December 2020 Publication History

Abstract

Modern aeroengine works under the harsh environment of higher temperature, higher pressure and higher speed, and the performance deteriorations of its components is inevitable. In this article, an adaptive hybrid fault-tolerant control (AHFTC) system is studied to deal with the concurrent faults of sensors and actuators during deterioration of engine components health parameters by fault-tolerant control. In this AHFTC system, the proposed estimation method using aeroengine thermodynamic nonlinear component-level (NCL) model merges the faults and deterioration estimation process and the fault-tolerant control process, so that it can greatly improve performance of the control system and reduce the processing time. The fault-tolerant controller in the AHFTC system can adjust its structure to adapt to different fault conditions. Simulation results of different scenarios show that the AHFTC system can minimize the influence of faults and maintain the performance of the engine when faults and health degradation coexist.

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Cited By

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  • (2024)Novel high-safety aeroengine performance predictive control method based on adaptive tracking weightChinese Journal of Aeronautics10.1016/j.cja.2024.03.01337:7(352-374)Online publication date: Jul-2024

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  1. An adaptive hybrid fault-tolerant control system design for aeroengine sensor and actuator faults

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    cover image ACM Other conferences
    RICAI '20: Proceedings of the 2020 2nd International Conference on Robotics, Intelligent Control and Artificial Intelligence
    October 2020
    470 pages
    ISBN:9781450388306
    DOI:10.1145/3438872
    Permission to make digital or hard copies of all or part of this work for personal or classroom use is granted without fee provided that copies are not made or distributed for profit or commercial advantage and that copies bear this notice and the full citation on the first page. Copyrights for components of this work owned by others than ACM must be honored. Abstracting with credit is permitted. To copy otherwise, or republish, to post on servers or to redistribute to lists, requires prior specific permission and/or a fee. Request permissions from [email protected]

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    Publication History

    Published: 25 December 2020

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    Author Tags

    1. Actuator fault
    2. Kalman filter
    3. fault-tolerant control
    4. onboard engine model
    5. sensor fault
    6. switching

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    • (2024)Novel high-safety aeroengine performance predictive control method based on adaptive tracking weightChinese Journal of Aeronautics10.1016/j.cja.2024.03.01337:7(352-374)Online publication date: Jul-2024

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