DocumentCode
1795209
Title
An improved EMD time-frequency analysis method for rocket vibration signal
Author
Zhang Jianhai ; Han Yingchun ; Li Lianzhou ; Liu Jun ; Che Bin
Author_Institution
State Key Lab. of Astronaut. Dynamics, Xi´an, China
fYear
2014
fDate
8-10 Aug. 2014
Firstpage
1842
Lastpage
1846
Abstract
According to noise and low frequency redundant problems generated by analyzing non-stationary signal with empirical mode decomposition (EMD) method, this paper proposes an improved EMD method which uses instantaneous frequency weighed average algorithm to eliminate noise component and correlate coefficient significant test to eliminate low redundant components. The improved EMD method which can obtain effective intrinsic mode function (IMF) from investigated signal was applied in simulation signal and rocket vibration signal to analyze time-frequency characteristics. The result indicates that this method can eliminate noise and low frequency redundant component effectively.
Keywords
noise; rockets; signal processing; time-frequency analysis; vibrations; EMD time-frequency analysis method; IMF; empirical mode decomposition; intrinsic mode function; low frequency redundant problems; noise component; nonstationary signal; rocket vibration signal; Analytical models; Frequency modulation; Noise; Rockets; Time-frequency analysis; Transforms; Vibrations;
fLanguage
English
Publisher
ieee
Conference_Titel
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location
Yantai
Print_ISBN
978-1-4799-4700-3
Type
conf
DOI
10.1109/CGNCC.2014.7007461
Filename
7007461
Link To Document