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Peaks Over Threshold Method for Structural Health Monitoring Detector Design

Communication avec acte
Auteur
HMAD, Ouadie
ccMECHBAL, Nazih
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]
ccRÉBILLAT, Marc

URI
http://hdl.handle.net/10985/10377
Date
2015

Résumé

Structural Health Monitoring (SHM) system offers new approaches to interrogate the integrity of structures. The most critical step of such systems is the damage detection step since it is the first and because performances of the following steps (damage localization, severity estimation…) depend on it. Care has thus to be taken when designing the detector. The objective of this communication is to discuss issues related to the design of a detector for the structural health monitoring of composite structures. The structure under monitoring is a substructure of an aircraft nacelle. In the absence of damage, the detector principle is to statistically characterize the healthy behavior of the structure. This characterization is based on the availability of a decision statistics synthesized from a damage index. Airline business models rely on Probability of False Alarms (Pfa) as main performance criterion. In general, the requirement on Pfa is 10E-9 which is very small. To determine the decision threshold, the approach we consider, consists to model the tail of the decision statistics using the Peaks Over Threshold method extracted from the extreme value theory (EVT). This method has been applied for different configuration of learning sample and probability of false alarm. This approach of tail distribution estimation is interesting since it is not necessary to know the distribution of the decision statistic to develop a detector. However, its main drawback is that it is necessary to have very large databases to accurately estimate decision thresholds to then decide the presence or absence of damage.

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Documents liés

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  • Peaks Over Threshold–based detector design for structural health monitoring: Application to aerospace structures 
    Article dans une revue avec comité de lecture
    HMAD, Ouadie; KADRI, Farid; ccMECHBAL, Nazih; ccRÉBILLAT, Marc (SAGE Publications (UK and US), 2018)
    Structural health monitoring offers new approaches to interrogate the integrity of complex structures. The structural health monitoring process classically relies on four sequential steps: damage detection, localization, ...
  • Verification and Validation of Structural Health Monitoring Algorithms: A Maturation Procedure 
    Communication avec acte
    HMAD, Ouadie; FENDZI, Claude; ccMECHBAL, Nazih; ccRÉBILLAT, Marc (IFAC, 2015)
    Structural Health Monitoring (SHM) system offers new approaches to interrogate the integrity of structures. However, their reliability has still to be demonstrated an quantified to enable confidence transition from R&D to ...
  • 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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