Abstract

In this paper, the problem of fault-tolerant control is investigated for turbofan engines with actuator faults. The controller involvement has repressed the effects of actuator faults on the controlled outputs of turbofan engines, making fault-tolerant control difficult. To solve this problem, the internal gas-path data of turbofan engines is introduced to provide conducive fault information. Besides, the useful property of the convolution neural network (CNN) is explored and utilized in fault-tolerant control. Based on the analysis of actuator faults, by using the Lyapunov stability and $L_{2}$ -gain like theorems, a novel CNN-based intelligent fault-tolerant control system for turbofan engines is proposed, including a CNN-based fault diagnosis module and a nonlinear fault-tolerant control with corresponding reconfiguration unit. The CNN-based intelligent fault-tolerant control system has the advantages of reducing the accuracy requirements of the mathematical description of turbofan engines. Furthermore, the proposed system can diagnose actuator faults and reduce the adverse effects of actuator faults on turbofan engines. Finally, simulation results are presented to demonstrate the efficiency of the designed method.

Highlights

  • In the event of actuator faults, the controlled outputs of turbofan engines are with small changes for a short time due to controller engagement [1]

  • SIMULATION RESULTS the effectiveness of the proposed CNN-based intelligent fault-tolerant control (CIFTC) system is verified for turbofan engines

  • To monitoring the engine operation, the gas-path total measurable fault information (GToMFI) database is employed for training and verifying the convolution neural network (CNN) diagnosis model

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Summary

Introduction

In the event of actuator faults, the controlled outputs of turbofan engines are with small changes for a short time due to controller engagement [1]. Fault-tolerant control plays a critical role in enhancing the safety and reliability of turbofan engines. The existing fault-tolerant control techniques of turbofan engines are categorized into two classes: passive approach and active approach [6], [7]. The parameters of the passive fault-tolerant control are selected overly conservatively such that the turbofan engines may have a loss of performance in the nominal case [8]. The active fault-tolerant controller can be reconfigured flexibly according to the faults information provided by the diagnosis module to reduce the conservation.

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