Recursive Method in Modal Parameter Identification of Aerospace Structures under Non-Gaussian Noise
Operational modal parameter identification is a tough problem in aerospace engineering due to the complex mechanics environment, various noises, and limited computational resources. In this paper, a novel, recursive, robust, and high-efficiency modal parameter identification approach is proposed for...
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| Main Authors: | Lei Yu, Yong-li Zhang, Meng-di Yuan, Rui-qing Liu, Qi Zhang |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2020-01-01
|
| Series: | Shock and Vibration |
| Online Access: | http://dx.doi.org/10.1155/2020/2946709 |
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