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Extrapolation of AR models using cubic splines for damage progression evaluation in composite structures

Article dans une revue avec comité de lecture
Auteur
DA SILVA, Samuel
225522 Universidade Estadual Paulista Júlio de Mesquita Filho = São Paulo State University [UNESP]
PAIXÃO, Jessé
225522 Universidade Estadual Paulista Júlio de Mesquita Filho = São Paulo State University [UNESP]
ccRÉBILLAT, Marc
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]
ccMECHBAL, Nazih
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]

URI
http://hdl.handle.net/10985/20458
DOI
10.1177/1045389x20963171
Date
2020
Journal
Journal of Intelligent Material Systems and Structures

Résumé

This paper presents the potentiality of the use of extrapolation of a set of Auto-Regressive (AR) models to inspect a future damage sensitive indices based on changes in one-step-ahead prediction errors. The key idea is to use multiple AR models to assess a data-driven model to represent and predict the time-series outputs of the PZT sensors receiving Lamb waves in a composite coupon. Based on some simplified assumptions, after detecting initial damage using some previous classifier, its progression evaluation by interpolating the AR parameters is proposed and examined based on cubic spline functions. After, an extrapolated AR model using this information may verify the future state and to inspect how the damage could progress. An aeronautical composite panel with bonded piezoelectric elements that act both as sensors and actuators is utilized to examine the relationship between the variation of the identified model parameters with various levels of simulated damage. The results have shown a smooth and adequate correlation between the estimates obtained by the extrapolated model and the actual progress of the damage observed. The significant advantage of the proposed procedure is implementing this task without adopting a complicated and costly mathematical-physical model.

Fichier(s) constituant cette publication

Nom:
PIMM_JMMS_DASILVA_2021
Taille:
1.932Mo
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Documents liés

Visualiser des documents liés par titre, auteur, créateur et sujet.

  • DATA-DRIVEN AUTOREGRESSIVE MODEL IDENTIFICATION FOR STRUCTURAL HEALTH MONITORING IN ANISOTROPIC COMPOSITE PLATES 
    Communication avec acte
    DA SILVA, Samuel; PAIXAO, Jessé; ccMECHBAL, Nazih; ccRÉBILLAT, Marc (A. Benjeddou, N. Mechbal and J.F. Deü, 2019)
    A simple data-driven AutoRegressive (AR) model may be used to assess a model to describe and to predict the time-series outputs of the PZT sensors receiving Lamb waves for different operating conditions in composite ...
  • MONITORING AND CONTROL OF STRUCTURES SUBJECT TO VIBRATION AND DAMAGE USING THE KOOPMAN OPERATOR 
    Communication sans acte
    THAIS COLOMBO, Fernanda; DA SILVA, Samuel; ccRÉBILLAT, Marc; ccMECHBAL, Nazih (2025-02)
    Due to the effects of fatigue and excessive vibration, structures may present a different health condition than initially observed. The change in system behavior due to damage also causes the system to demand more energy, ...
  • Gaussian Process NARX Model for Damage Detection in Composite Aircraft Structures 
    Article dans une revue avec comité de lecture
    DA SILVA, Samuel; VILLANI, Luis G. G.; ccRÉBILLAT, Marc; ccMECHBAL, Nazih (ASME International, 2021-12)
    This article demonstrates the Gaussian process regression model’s applicability combined with a nonlinear autoregressive exogenous (NARX) framework using experimental data measured with PZTs’ patches bonded in a composite ...
  • In-situ monitoring of µm-sized electrochemically generated corrosion pits using Lamb Waves managed by a sparse array of piezoelectric transducers 
    Communication sans acte
    ccRÉBILLAT, Marc; ccNICARD, Cyril; ccDEVOS, Olivier; ccEL MAY, Mohamed; LETELLIER, Frédéric; THOMACHOT, Matthieu; FOURNIER, Marc; ccMECHBAL, Nazih (2024-09)
    al components, roughening the outer surface, loosening fasteners, hastening cracking, and facilitating the entry of water into electronic fixtures. In 2016, the combined commercial aircraft fleet operated by European ...
  • Improving Lamb Wave detection for SHM using a dedicated LWDS electronics 
    Communication avec acte
    JAUSSAUD, Gladys; REBUFA, Jocelyn; FOURNIER, Marc; LOGEAIS, Matthieu; BENCHEIKH, Nabil; ccMECHBAL, Nazih; ccRÉBILLAT, Marc (NTD, 2019)
    In the context of Condition Based Maintenance (CBM) for aircrafts, Structural Health Monitoring (SHM) is one main field of research. Detection and localization of damages in a structure request reliability of the equipment ...

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