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http://dx.doi.org/10.12989/sss.2015.16.3.435

Perturbation analysis for robust damage detection with application to multifunctional aircraft structures  

Hajrya, Rafik (Arts et Metiers ParisTech (ENSAM), Process and Engineering in Mechanics and Materials Laboratory (PIMM))
Mechbal, Nazih (Arts et Metiers ParisTech (ENSAM), Process and Engineering in Mechanics and Materials Laboratory (PIMM))
Publication Information
Smart Structures and Systems / v.16, no.3, 2015 , pp. 435-457 More about this Journal
Abstract
The most widely known form of multifunctional aircraft structure is smart structures for structural health monitoring (SHM). The aim is to provide automated systems whose purposes are to identify and to characterize possible damage within structures by using a network of actuators and sensors. Unfortunately, environmental and operational variability render many of the proposed damage detection methods difficult to successfully be applied. In this paper, an original robust damage detection approach using output-only vibration data is proposed. It is based on independent component analysis and matrix perturbation analysis, where an analytical threshold is proposed to get rid of statistical assumptions usually performed in damage detection approach. The effectiveness of the proposed SHM method is demonstrated numerically using finite element simulations and experimentally through a conformal load-bearing antenna structure and composite plates instrumented with piezoelectric ceramic materials.
Keywords
structural health monitoring; robust damage detection; decision-making; analytical threshold; matrix perturbation theory; range subspaces; independent component analysis; piezoelectric ceramic material; composite structures; conformal load-bearing antenna structure; impact damages;
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Times Cited By KSCI : 2  (Citation Analysis)
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