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Operational modal parameter identification with colored noise excitation
- Source :
- Chinese Journal of Aeronautics, Vol 34, Iss 2, Pp 288-300 (2021)
- Publication Year :
- 2021
- Publisher :
- Elsevier, 2021.
-
Abstract
- Operational Modal Analysis (OMA) refers to the modal analysis of a structure in its operating state. The advantage of OMA is that only the output vibration signal of a system is used in the analysis process. Classic OMA is based on the white noise excitation assumption and many identification methods have been developed in both time domain and frequency domain. But in reality, many environmental excitations are not compliance with the white noise assumption. In this paper, a method of half power bandwidth analysis is applied to power spectrum analysis to deal with the colored noise and trapezoidal spectral excitation. The modal frequencies and modal damping ratios are derived and the error caused by trapezoidal spectral and colored noise excitation are analyzed. It is proved that the OMA algorithm based on the white noise assumption can be extended to the colored noise environments under certain conditions. Finally, a simulation example with a cantilever beam and a vibration test with four kinds of colored noise and trapezoidal spectrum base excitation are carried out and the results support the proposed method.
- Subjects :
- 0209 industrial biotechnology
Computer science
Mechanical Engineering
Acoustics
Modal analysis
Aerospace Engineering
Spectral density
Operational Modal Analysis
Modal parameter identification
TL1-4050
02 engineering and technology
White noise
Trapezoidal spectrum
Colored noise
01 natural sciences
010305 fluids & plasmas
020901 industrial engineering & automation
Modal
Colors of noise
Half power bandwidth
Frequency domain
0103 physical sciences
Time domain
Motor vehicles. Aeronautics. Astronautics
Subjects
Details
- Language :
- English
- ISSN :
- 10009361
- Volume :
- 34
- Issue :
- 2
- Database :
- OpenAIRE
- Journal :
- Chinese Journal of Aeronautics
- Accession number :
- edsair.doi.dedup.....d8883a4a5a3552606b2902170ea0107c