Aero-Engine On-Board Model Based on Batch Normalize Deep Neural Network

A new on-board turbo-fan engine modeling method based on a batch normalize (BN) mini-batch gradient descent (MGD) deep neural network (NN) is proposed. This new method adopts BN algorithm, which accelerates the network training speed and overcomes the gradient vanish problem. Hence, using the BN alg...

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Main Authors: Qiangang Zheng, Juan Fang, Zhongzhi Hu, Haibo Zhang
Format: Article
Language:English
Published: IEEE 2019-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/8704262/
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spelling doaj-f9c111e90e654b0fa24ebabb4ad5e6e22021-03-29T22:40:36ZengIEEEIEEE Access2169-35362019-01-017548555486210.1109/ACCESS.2018.28851998704262Aero-Engine On-Board Model Based on Batch Normalize Deep Neural NetworkQiangang Zheng0https://orcid.org/0000-0002-8055-5633Juan Fang1Zhongzhi Hu2Haibo Zhang3Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing, ChinaJiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing, ChinaJiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing, ChinaJiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing, ChinaA new on-board turbo-fan engine modeling method based on a batch normalize (BN) mini-batch gradient descent (MGD) deep neural network (NN) is proposed. This new method adopts BN algorithm, which accelerates the network training speed and overcomes the gradient vanish problem. Hence, using the BN algorithm, the neural network adopts the deeper structure, which means the network has a stronger representation capacity. This mini-batch gradient descent (MGD-NN) algorithm that consumes much less time to update the NN parameters is adopted. Therefore, it is more suitable for training big dataset and establishing a high-accuracy engine model in a large flight envelope. Finally, to verify whether the proposed method could be applied to larger flight envelope, the conventional NN also adopts MGD (called MGD-NN). The turbo-fan engine models based on these two modeling methods are both conducted within a sub-sonic cruise envelope. The simulation results show that the proposed modeling method has much higher accuracy than the MGD-NN. Moreover, the proposed method has the characteristics of less data storage, low computation complexity, and good real-time performance, which are the most importance indices for model realize on-board.https://ieeexplore.ieee.org/document/8704262/Aero-engine modelbatch normalizedeep neural networkturbo-fan on-board modelmini-batch gradient descentdata storage
collection DOAJ
language English
format Article
sources DOAJ
author Qiangang Zheng
Juan Fang
Zhongzhi Hu
Haibo Zhang
spellingShingle Qiangang Zheng
Juan Fang
Zhongzhi Hu
Haibo Zhang
Aero-Engine On-Board Model Based on Batch Normalize Deep Neural Network
IEEE Access
Aero-engine model
batch normalize
deep neural network
turbo-fan on-board model
mini-batch gradient descent
data storage
author_facet Qiangang Zheng
Juan Fang
Zhongzhi Hu
Haibo Zhang
author_sort Qiangang Zheng
title Aero-Engine On-Board Model Based on Batch Normalize Deep Neural Network
title_short Aero-Engine On-Board Model Based on Batch Normalize Deep Neural Network
title_full Aero-Engine On-Board Model Based on Batch Normalize Deep Neural Network
title_fullStr Aero-Engine On-Board Model Based on Batch Normalize Deep Neural Network
title_full_unstemmed Aero-Engine On-Board Model Based on Batch Normalize Deep Neural Network
title_sort aero-engine on-board model based on batch normalize deep neural network
publisher IEEE
series IEEE Access
issn 2169-3536
publishDate 2019-01-01
description A new on-board turbo-fan engine modeling method based on a batch normalize (BN) mini-batch gradient descent (MGD) deep neural network (NN) is proposed. This new method adopts BN algorithm, which accelerates the network training speed and overcomes the gradient vanish problem. Hence, using the BN algorithm, the neural network adopts the deeper structure, which means the network has a stronger representation capacity. This mini-batch gradient descent (MGD-NN) algorithm that consumes much less time to update the NN parameters is adopted. Therefore, it is more suitable for training big dataset and establishing a high-accuracy engine model in a large flight envelope. Finally, to verify whether the proposed method could be applied to larger flight envelope, the conventional NN also adopts MGD (called MGD-NN). The turbo-fan engine models based on these two modeling methods are both conducted within a sub-sonic cruise envelope. The simulation results show that the proposed modeling method has much higher accuracy than the MGD-NN. Moreover, the proposed method has the characteristics of less data storage, low computation complexity, and good real-time performance, which are the most importance indices for model realize on-board.
topic Aero-engine model
batch normalize
deep neural network
turbo-fan on-board model
mini-batch gradient descent
data storage
url https://ieeexplore.ieee.org/document/8704262/
work_keys_str_mv AT qiangangzheng aeroengineonboardmodelbasedonbatchnormalizedeepneuralnetwork
AT juanfang aeroengineonboardmodelbasedonbatchnormalizedeepneuralnetwork
AT zhongzhihu aeroengineonboardmodelbasedonbatchnormalizedeepneuralnetwork
AT haibozhang aeroengineonboardmodelbasedonbatchnormalizedeepneuralnetwork
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