Gaussian process modeling for damage detection in composite aerospace structures by using discrete strain measurements

Joham Alvarez-Montoya, M. A. Torres-Arredondo, Julián Sierra-Pérez

    Resultado de la investigación: Capítulo del libro/informe/acta de congresoContribución a la conferenciarevisión exhaustiva

    1 Cita (Scopus)

    Resumen

    The first approaches to damage detection in the context of Structural Health Monitoring (SHM) focused on identification techniques based on physical models, which imply the need of a model to describe the relationship between actions and responses in the structure. However, in the case of aerospace structures, where complex designs and materials are used to accomplish the demanding requirements, it is difficult to estimate accurate models to be used for diagnosis in aircraft Health and Usage Monitoring Systems (HUMS). This is even more evident with the increased use of composite materials in the aerospace industry. In this way, data-driven models which are based only on experimental data have been successfully implemented. Such techniques use machine learning algorithms to "learn" and evaluate the structural integrity with high accuracy. In previous work, the authors have developed a methodology based on Self-Organizing Maps (SOM) and Principal Component Analysis (PCA) for this kind of structures. Suitable results were obtained for strain data acquired from an Unmanned Aerial Vehicle (SMARP UAV) in flight tests by means of 20 Fiber Bragg Grating (FBG) sensors. However, there are different existing machine learning techniques that can be applied to develop novel methodologies for this kind of structures. One promising approach is Gaussian Process (GP) modeling, which can be seen as a generalization of a Gaussian distribution, adapted to classification problems for diagnosis. The main advantage of using this type of modeling is its well-founded approach to deal with the learning and model selection problem. Therefore, the aim of this work is to evaluate a methodology for damage detection in aerospace structures based on GP modeling by means of discrete strain measurements. The performance of the methodology is evaluated by using Receiver Operating Characteristic (ROC) curve analysis achieving a F1 score of about 0.944 in the best case.

    Idioma originalInglés
    Título de la publicación alojadaProceedings of the 7th Asia-Pacific Workshop on Structural Health Monitoring, APWSHM 2018
    EditoresZhongqing Su, Shenfang Yuan, Hoon Sohn
    EditorialNDT.net
    Páginas710-718
    Número de páginas9
    ISBN (versión digital)9783000603594
    EstadoPublicada - 2018
    Evento7th Asia-Pacific Workshop on Structural Health Monitoring, APWSHM 2018 - Hong Kong, China
    Duración: 12 nov. 201815 nov. 2018

    Serie de la publicación

    NombreProceedings of the 7th Asia-Pacific Workshop on Structural Health Monitoring, APWSHM 2018

    Conferencia

    Conferencia7th Asia-Pacific Workshop on Structural Health Monitoring, APWSHM 2018
    País/TerritorioChina
    CiudadHong Kong
    Período12/11/1815/11/18

    Nota bibliográfica

    Publisher Copyright:
    © APWSHM 2018. All rights reserved.

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