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Automatic Damage Quantification Using Signal Based And Nonlinear Model Based Damage Sensitive Features

Communication avec acte
Auteur
GHRIB, Meriem
VERMOT DES ROCHES, Guillaume
175453 Arts et Métiers ParisTech
ccMECHBAL, Nazih
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]
ccRÉBILLAT, Marc

URI
http://hdl.handle.net/10985/12043
Date
2017

Résumé

Structural Health Monitoring (SHM) can be de ned as the process of acquiring and analyzing data from on-board sensors to evaluate the health of a structure. Classically, an SHM process can be performed in four steps: detection, localization, classi cation and quanti cation. This paper addresses damage quanti cation issue as a classi cation problem whereby each class corresponds to a certain damage extent. Starting from the assumption that damage causes a structure to exhibit nonlinear response, we investigate whether the use of nonlinear model based features increases classi cation performance. A support Vector Machine (SVM) is used to perform multi-class classi cation task. Two types of features are used as inputs to the SVM algorithm: Signal Based Features (SBF) and Nonlinear Model Based Features (NMBF). SBF are rooted in a direct use of response signals and do not consider any underlying model of the test structure. NMBF are computed based on parallel Hammerstein models which are identi ed with an Exponential Sine Sweep (ESS) signal. A study of the sensitivity of classi cation performance to the noise contained in output signals is also conducted. Dimension reduction of features vector using Principal Component Analysis (PCA) is carried out in order to nd out if it allows robustifying the quanti cation process suggested in this work. Simulation results on a cantilever beam with a bilinear torsion spring sti ness are considered for demonstration. Results show that by introducing NMBF, classi cation performance is improved. Furthermore, PCA allows for higher recognition rates while reducing features vector dimension. However, classi ers trained on NMBF or on principal components appear to be more sensitive to output noise than those trained on SBF.

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Documents liés

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  • Automatic damage type classification and severity quantification using signal based and nonlinear model based damage sensitive features 
    Article dans une revue avec comité de lecture
    GHRIB, Meriem; ccRÉBILLAT, Marc; VERMOT DES ROCHES, Guillaume; ccMECHBAL, Nazih (Elsevier, 2019)
    Structural health monitoring (SHM) is an emerging technology designed to automate the inspectionprocess undertaken to assess the health condition of structures. The SHM process is classically decom-posed into four sequential ...
  • Laser shock a novel way to generate calibrated delamination in composites: concept and first results 
    Communication avec acte
    GHRIB, Meriem; BERTHE, Laurent; ECAULT, Romain; ccMECHBAL, Nazih; ccGUSKOV, Mikhail; ccRÉBILLAT, Marc (2015)
    Structural Health Monitoring (SHM) has been gaining importance in recent years. SHM aims at providing structures with similar functionality as the biological nervous system and it is organized into four main steps: detection, ...
  • Signal-based versus nonlinear model-based damage sensitive features for delamination quantification in CFRP composites 
    Communication avec acte
    GHRIB, Meriem; BERTHE, Laurent; ccMECHBAL, Nazih; ccGUSKOV, Mikhail; ccRÉBILLAT, Marc (2017)
    Structural health monitoring (SHM) is an emerging technology designed to automate the inspection process undertaken to assess the health condition of structures. The SHM process is classically decomposed into four sequential ...
  • Generation of controlled delaminations in composites using symmetrical laser shock configuration 
    Article dans une revue avec comité de lecture
    GHRIB, Meriem; BERTHE, Laurent; ECAULT, Romain; BEDREDDINE, Nas; ccMECHBAL, Nazih; ccGUSKOV, Mikhail; ccRÉBILLAT, Marc (Elsevier, 2017)
    Structural Health Monitoring (SHM) is defined as the process of implementing a damage identification strategy for aerospace, civil and mechanical engineering infrastructures. SHM can be organized into five main steps: ...
  • LASER shock delamination generation and machine learning-based damage quantification in CFRP composites plates 
    Communication avec acte
    GHRIB, Meriem; BERTHE, Laurent; ccMECHBAL, Nazih; ccGUSKOV, Mikhail; ccRÉBILLAT, Marc (A. Benjeddou and Z. Aboura, 2018)
    In the aeronautic industry, composite materials are becoming more widespread due to their high strength to mass ratio. Piezoelectric elements can be permanently incorporated on composite parts during the manufacturing ...

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