Full Text

Turn on search term navigation

© 2024 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.

Abstract

With the continuous development of actuator technology, the Electro-Mechanical Actuator (EMA) is gradually becoming the first choice in the aviation field. Permanent Magnet Synchronous Motor (PMSM) is one of the core components of EMA, and its healthy state determines the working performance of EMA. In this paper, the interturn short-circuit fault of PMSM is taken as the typical fault, and a new fault diagnosis framework is proposed based on a wide-kernel convolutional neural network (WCNN) and few-shot learning. Firstly, the wide convolution kernel is added as the first layer to extract short-time features while automatically learning deeply oriented features oriented to diagnosis and removing useless features. Then, the twin neural network is introduced to establish a wide kernel convolutional neural network, which can also achieve good diagnostic results under a few-shot learning framework. The effectiveness of the proposed method is verified by the general data set. The results show that the accuracy of few-shot learning is 9% higher than that of WCNN when the fault data are small. Finally, a fault test platform was built for EMA to collect three-phase current data under different fault states, and the collected data were used to complete the fault diagnosis of PMSM. With limited data, the accuracy of few-shot learning increased by 8% on average compared with WCNN, which has good engineering value.

Details

Title
Fault Diagnosis Method of Permanent Magnet Synchronous Motor Based on WCNN and Few-Shot Learning
Author
Zhang, Chao 1 ; Wang, Fei 2 ; Li, Xiangzhi 3 ; Dong, Zhijie 4 ; Zhang, Yubo 5 

 Department of Integrated Technology and Control Engineering, School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, China; [email protected]; National Key Laboratory of Aircraft Design, Xi’an 710072, China 
 Department of Integrated Technology and Control Engineering, School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, China; [email protected] 
 AVIC Chengdu Kaitian Electronics Co., Ltd., Chengdu 610091, China; [email protected] 
 The 6th Research Institute of China Electronics Corporation, Beijing 102209, China; [email protected] 
 AVIC Xi’an Flight Automatic Control Research Institute, Xi’an 710065, China; [email protected] 
First page
373
Publication year
2024
Publication date
2024
Publisher
MDPI AG
ISSN
20760825
Source type
Scholarly Journal
Language of publication
English
ProQuest document ID
3110278631
Copyright
© 2024 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.