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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Bibliographic Details
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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