DocumentCode :
3319199
Title :
Adaptive de-noising of defect signal of aerospace launcher steel structure based on EEMD
Author :
Li Wei ; Zuo Xianzhang ; Li Jianzeng ; Meng Wei
Author_Institution :
Dept. of UAV Eng., Ordnance Eng. Coll., Shijiazhuang, China
Volume :
1
fYear :
2013
fDate :
16-19 Aug. 2013
Firstpage :
1
Lastpage :
4
Abstract :
This paper proposes a kind of adaptive noise cancellation method based on EEMD that considers the non-stationary and weak of defect signal of aerospace launcher steel structure. First, the non-stationary defect signals are adaptively decomposed according to EEMD. It can effectively inhibit the folding phenomenon of model that may appear in classical empirical mode decomposition. Then, the product of energy density and average period of IMF components is a constant value. On the basis of the constant value, it can automatically eliminate the decomposed intrinsic mode function. Finally, the signals upon commands from the rest IMF components are reconstituted. The results show that an adaptive de-noising method based on EEMD is fully data-driven, it has more adaptive ability than empirical mode decomposition de-noising method. In conclusion, this method is more conducive to the de-noising of defect signal of the aerospace launcher steel structure.
Keywords :
aerospace materials; aerospace testing; decomposition; noise abatement; signal denoising; steel; EEMD; IMF component; adaptive defect signal denoising; adaptive noise cancellation method; aerospace launcher steel structure; aerospace material; aerospace testing; empirical mode decomposition; energy density; intrinsic mode function decomposition; Empirical mode decomposition; Instruments; Machinery; Noise reduction; Steel; White noise; EEMD; aerospace launcher; signal de-noising;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electronic Measurement & Instruments (ICEMI), 2013 IEEE 11th International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4799-0757-1
Type :
conf
DOI :
10.1109/ICEMI.2013.6743003
Filename :
6743003
Link To Document :
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