王慧, 郭晨林, 王乐, 张敏照. 基于内积矩阵及深度学习的结构健康监测研究[J]. 工程力学, 2022, 39(2): 14-22, 75. DOI: 10.6052/j.issn.1000-4750.2020.12.0935
引用本文: 王慧, 郭晨林, 王乐, 张敏照. 基于内积矩阵及深度学习的结构健康监测研究[J]. 工程力学, 2022, 39(2): 14-22, 75. DOI: 10.6052/j.issn.1000-4750.2020.12.0935
WANG Hui, GUO Chen-lin, WANG Le, ZHANG Min-zhao. STRUCTURAL HEALTH MONITORING BASED ON INNER PRODUCT MATRIX AND DEEP LEARNING[J]. Engineering Mechanics, 2022, 39(2): 14-22, 75. DOI: 10.6052/j.issn.1000-4750.2020.12.0935
Citation: WANG Hui, GUO Chen-lin, WANG Le, ZHANG Min-zhao. STRUCTURAL HEALTH MONITORING BASED ON INNER PRODUCT MATRIX AND DEEP LEARNING[J]. Engineering Mechanics, 2022, 39(2): 14-22, 75. DOI: 10.6052/j.issn.1000-4750.2020.12.0935

基于内积矩阵及深度学习的结构健康监测研究

STRUCTURAL HEALTH MONITORING BASED ON INNER PRODUCT MATRIX AND DEEP LEARNING

  • 摘要: 环境激励下仅利用振动响应的结构健康监测方法,因其便于实现在线监测受到了越来越多的关注。该文回顾了以振动时域响应相关性分析为基础的结构特征参数(即内积向量)的基本概念及特征。为了从已有测试数据中提取更多的结构特征参数,分别以各个响应测点为参考点来构建多个内积向量并组成矩阵,将内积向量扩展到了内积矩阵。进而以内积矩阵为结构特征参数,结合深度卷积神经网络的特征提取能力,提出了基于内积矩阵及深度学习的结构健康监测方法。典型航空加筋壁板螺栓松动监测的实验研究结果表明,仅利用结构在环境激励下部分测点的振动时域响应,该文方法可以准确地识别螺栓松动位置。

     

    Abstract: Structural health monitoring methods using vibration responses only under ambient excitation are appealing as its convenience to realize on-line monitoring. The basic concepts and characteristics of structural characteristic parameter (i.e. inner product vector) based on the correlation analysis of time domain vibration response are reviewed. In order to extract more structural characteristic parameters from the existing test data, the inner product vector is extended to the inner product matrix by using several inner product vectors which are constructed by setting each measurement point as the reference measurement point. Furthermore, taking the inner product matrix as the structural characteristic parameter and combining the feature extraction ability of deep convolution neural network, a structural health monitoring method based on deep learning and inner product matrix is proposed. The experimental results of monitoring the bolt loosening of a typical aeronautical stiffened panel show that the bolt loosening position can be correctly located using the time domain vibration response only under ambient excitation.

     

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