Structural fault diagnosis of UAV based on convolutional neural network and data processing technology

被引:9
|
作者
Ma, Yumeng [1 ,2 ,3 ]
Mustapha, Faizal [1 ]
Ishak, Mohamad Ridzwan [1 ,4 ,5 ]
Rahim, Sharafiz Abdul [6 ]
Mustapha, Mazli [7 ]
机构
[1] Univ Putra Malaysia, Fac Engn, Dept Aerosp Engn, Serdang, Selangor, Malaysia
[2] BinZhou Univ, Coll Aeronaut Engn, Binzhou, Shandong, Peoples R China
[3] BinZhou Univ, Engn Res Ctr Aeronaut Mat & Devices Aeronaut Engn, Binzhou, Shandong, Peoples R China
[4] Univ Putra Malaysia, Fac Engn, Aerosp Malaysia Res Ctr AMRC, Serdang, Selangor, Malaysia
[5] Univ Putra Malaysia, Inst Trop Forestry & Forest Prod INTROP, Lab Biocomposite Technol, Serdang, Selangor, Malaysia
[6] Univ Putra Malaysia, Fac Engn, Dept Mech & Mfg Engn, Serdang, Selangor, Malaysia
[7] Univ Teknol PETRONAS, Dept Mech Engn, Iskandar, Perak, Malaysia
关键词
Multi-rotor UAV; Damage detection and identification; Vibration data acquisition; Deep learning; CNN; DAMAGE DETECTION; IDENTIFICATION; CNN;
D O I
10.1080/10589759.2023.2206655
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
This study presents a novel method for damage detection and identification in unmanned aerial vehicles (UAVs) using vibration data gathering and processing technologies based on deep learning. To conduct the study, a quad-rotor UAV was manufactured, and a vibration data acquisition system was developed to collect vibration data along three axes under normal and three damage scenarios. Empirical mode decomposition (EMD) was employed to reduce high-frequency noise in the signals, and the root mean square error (RMSE) feature was utilised to select the Y-axis acceleration data, which exhibits significant changes across different damage cases. Finally, a convolutional neural network was used to identify the damage based on the vibration data. Experimental results demonstrate that the proposed method achieved 97.5% accuracy using selected and noise-reduced Y-axis acceleration data, thereby indicating its usefulness in diagnosing damage types in multi-rotor UAVs.
引用
收藏
页码:426 / 445
页数:20
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