Aircraft classification method based on the kurtosis-skewness feature and wavelet decomposition and linear discriminant analysis

被引:2
作者
Kang, Pengpeng [1 ]
Chen, Zhiming [1 ]
机构
[1] Nanjing Res Inst Elect Technol, Nanjing 210012, Jiangsu, Peoples R China
来源
JOURNAL OF ENGINEERING-JOE | 2019年 / 2019卷 / 21期
关键词
statistical analysis; spectral analysis; noise; feature extraction; jet engines; wavelet transforms; modulation; image classification; pattern classification; linear discriminant analysis; jet engine modulation feature; extraction methods; modulation wave period; inter-spectral interval; modulation line spectrum; spectral estimation methods; signal-to-noise ratio; PRF; observation time; aircraft target echoes; normalised amplitude distribution; kurtosis; skewness feature; strong anti-noise capability; aircraft classification method; wavelet decomposition; MICRO-DOPPLER SIGNATURES; RADAR;
D O I
10.1049/joe.2019.0679
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
At present, most of the jet engine modulation feature extraction methods are based on the modulation wave period or the inter-spectral interval of the modulation line spectrum. However, such spectral estimation methods are often difficult to obtain good classification performance due to the signal-to-noise ratio, pulse repetition frequency (PRF) and observation time. The statistical analysis of the three types of aircraft target echoes shows that there is a significant difference in the normalised amplitude distribution, and based on this, the kurtosis-skewness feature is extracted to classify the targets. This feature has a strong anti-noise capability, the requirement for PRF and observation time is not high, and one of the parameters can be used to make up for another parameter, so we can make a balance between PRF and time if needed. The simulation test proves that the proposed method has good classification performance.
引用
收藏
页码:7855 / 7859
页数:5
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