2019
DOI: 10.1049/iet-smt.2018.5226
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Feature extraction approach insensitive to temperature variations for impedance‐based structural health monitoring

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Cited by 10 publications
(4 citation statements)
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“…Structural health monitoring (SHM) has been considered a revolutionary technology for the operation and maintenance of aircraft structures [ 1 ]. At present, some SHM technologies, such as acoustic emission [ 2 , 3 ], eddy current [ 4 , 5 , 6 ], Lamb wave [ 7 , 8 ], impedance [ 9 , 10 ], vibration [ 11 , 12 ], and comparative vacuum [ 13 ] monitoring, have received greatly focused research and development for damage detection in aircraft structures. Lamb wave-based damage imaging, which is an active detection technology suitable for large-scale structures, is a promising technology for the health monitoring of aircraft plate structures [ 14 , 15 ].…”
Section: Introductionmentioning
confidence: 99%
“…Structural health monitoring (SHM) has been considered a revolutionary technology for the operation and maintenance of aircraft structures [ 1 ]. At present, some SHM technologies, such as acoustic emission [ 2 , 3 ], eddy current [ 4 , 5 , 6 ], Lamb wave [ 7 , 8 ], impedance [ 9 , 10 ], vibration [ 11 , 12 ], and comparative vacuum [ 13 ] monitoring, have received greatly focused research and development for damage detection in aircraft structures. Lamb wave-based damage imaging, which is an active detection technology suitable for large-scale structures, is a promising technology for the health monitoring of aircraft plate structures [ 14 , 15 ].…”
Section: Introductionmentioning
confidence: 99%
“…The experimental results indicated that the proposed variable F increases the robustness of the damage detection as compared to the quantities R and G, which demonstrated the effectiveness of the methodology. Campos et al [ 23 ] proposed a feature extraction approach insensitive to temperature variation for the impedance-based SHM technique. This study presents a new feature extraction approach that is insensitive to temperature variations.…”
Section: Introductionmentioning
confidence: 99%
“…ZnO PENG piezoelectric properties should be studied as a function of temperature if they are meant to be used at temperatures higher than room temperature. As the temperature of the PENG changes, its piezoelectric properties and impedance will change as well [109,110]. As a result, the optimal resistance value for maximum power transfer will change [109,110].…”
mentioning
confidence: 99%
“…As the temperature of the PENG changes, its piezoelectric properties and impedance will change as well [109,110]. As a result, the optimal resistance value for maximum power transfer will change [109,110].…”
mentioning
confidence: 99%