中国航空学报(英文版)2024,Vol.37Issue(1) :106-117.DOI:10.1016/j.cja.2023.09.001

Aeroengine thrust estimation and embedded verification based on improved temporal convolutional network

Wanzhi MENG Zhuorui PAN Sixin WEN Pan QIN Ximing SUN
中国航空学报(英文版)2024,Vol.37Issue(1) :106-117.DOI:10.1016/j.cja.2023.09.001

Aeroengine thrust estimation and embedded verification based on improved temporal convolutional network

Wanzhi MENG 1Zhuorui PAN 1Sixin WEN 1Pan QIN 1Ximing SUN1
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作者信息

  • 1. Key Laboratory of Intelligent Control and Optimization for Industrial Equipment of Ministry of Education,Dalian University of Technology,Dalian 116024,China School of Control Science and Engineering,Dalian University of Technology,Dalian 116024,China
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Abstract

Thrust estimation is a significant part of aeroengine thrust control systems.The tradi-tional estimation methods are either low in accuracy or large in computation.To further improve the estimation effect,a thrust estimator based on Multi-layer Residual Temporal Convolutional Network(M-RTCN)is proposed.To solve the problem of dead Rectified Linear Unit(ReLU),the proposed method uses the Gaussian Error Linear Unit(GELU)activation function instead of ReLU in residual block.Then the overall architecture of the multi-layer convolutional network is adjusted by using residual connections,so that the network thrust estimation effect and memory consumption are further improved.Moreover,the comparison with seven other methods shows that the proposed method has the advantages of higher estimation accuracy and faster convergence speed.Furthermore,six neural network models are deployed in the embedded controller of the micro-turbojet engine.The Hardware-in-the-Loop(HIL)testing results demonstrate the superiority of M-RTCN in terms of estimation accuracy,memory occupation and running time.Finally,an ignition verification is conducted to confirm the expected thrust estimation and real-time perfor-mance.

Key words

Thrust estimation/Temporal convolutional net-work/Embedded deployment/Hardware-in-the-loop test-ing/Ignition verification

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基金项目

National Natural Science Foundation of China(61890920)

National Natural Science Foundation of China(61890921)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量1
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