4.6 Article

Multi-Dimensional Uniform Initialization Gaussian Mixture Model for Spar Crack Quantification under Uncertainty

Journal

SENSORS
Volume 21, Issue 4, Pages -

Publisher

MDPI
DOI: 10.3390/s21041283

Keywords

structural health monitoring; guided wave; Gaussian mixture model; crack quantification; uncertainty; time-varying conditions

Funding

  1. National Natural Science Foundation of China [51921003, 51635008, 51905266]
  2. Jiangsu Provincial Key Research and Development Program of China [BE2018123]
  3. Priority Academic Program Development of Jiangsu Higher Education Institutions of China

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This paper investigates the use of Gaussian mixture models (GMM) for crack monitoring, proposing a multi-dimensional uniform initialization GMM method. By integrating multi-channel GW features to increase accuracy and stability in crack quantification, the research addresses the challenges of crack sensitivity in GW features and uncertainties in crack initiation and growth.
Guided Wave (GW)-based crack monitoring method as a promising method has been widely studied, as this method is sensitive to small cracks and can cover a wide monitoring range. Online crack quantification is difficult as the initiation and growth of crack are affected by various uncertainties. In addition, crack-sensitive GW features are influenced by time-varying conditions which further increase the difficulty in crack quantification. Considering these uncertainties, the Gaussian mixture model (GMM) is studied to model the probability distribution of GW features. To further improve the accuracy and stability of crack quantification under uncertainties, this paper proposes a multi-dimensional uniform initialization GMM. First, the multi-channel GW features are integrated to increase the accuracy of crack quantification, as GW features from different channels have different sensitivity to cracks. Then, the uniform initialization method is adopted to provide more stable initial parameters in the expectation-maximization algorithm. In addition, the relationship between the probability migration index of GMMs and crack length is calibrated with fatigue tests on prior specimens. Finally, the proposed method is applied for online crack quantification on the notched specimen of an aircraft spar with complex fan-shaped cracks under uncertainty.

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