Aero Engine Fault Diagnosis Based on Support Vector Machine

In order to improve the accuracy and efficiency of aero-engine fault diagnosis, support vector machine (SVM) technology is used in this study. SVM as a powerful supervised learning model, performs well in classification and regression problems, especially for dealing with high-dimensional data and complex nonlinear relationships. In this paper, the process of data acquisition and preprocessing is described first, and then the influence of different kernel functions on the model performance is discussed in the process of SVM model construction, and the optimal model parameters are determined by cross-validation and other methods. In the part of experiment setting, the key information such as experimental environment, data set division and performance evaluation index are explained in detail. Experimental results show that compared with traditional methods, the SVM based aero engine fault diagnosis method has significantly improved the fault identification accuracy and diagnosis speed.

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Publication Details

Journal
Procedia Computer Science
Published
2025-01-01
DOI
https://doi.org/10.1016/j.procs.2025.05.181
Citations
4
Primary Topic
Advanced Sensor and Control Systems
Type
article
Field-Weighted Citation Impact
4.86
Controls
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article

Aero Engine Fault Diagnosis Based on Support Vector Machine

Xiaoyu Wang
4 citations
Procedia Computer Science
Advanced Sensor and Control Systems
4.86
article

Aero Engine Fault Diagnosis Based on Support Vector Machine

Xiaoyu Wang
article en
4 citations

Abstract

In order to improve the accuracy and efficiency of aero-engine fault diagnosis, support vector machine (SVM) technology is used in this study. SVM as a powerful supervised learning model, performs well in classification and regression problems, especially for dealing with high-dimensional data and complex nonlinear relationships. In this paper, the process of data acquisition and preprocessing is described first, and then the influence of different kernel functions on the model performance is discussed in the process of SVM model construction, and the optimal model parameters are determined by cross-validation and other methods. In the part of experiment setting, the key information such as experimental environment, data set division and performance evaluation index are explained in detail. Experimental results show that compared with traditional methods, the SVM based aero engine fault diagnosis method has significantly improved the fault identification accuracy and diagnosis speed.

Procedia Computer ScienceVol. 262
Shanghai Civil Aviation College (CN)
Openalex Percentile: Top 5%
Advanced Sensor and Control Systems
4.86
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