Guided wave signal processing and image fusion for in situ damage localization in plates

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Piezoelectric Transducer-Based Structural Health Monitoring for Aircraft Applications (2019, methodology): “For example, Budoya and Baptista [25] used two measurements, i.e., transient-state measurement using a sweep excitation signal for all the components of the desired frequency range, and steady-state measurement using a pure sinusoidal signal for each frequency of interest.”
Simulation Methods for Guided Wave-Based Structural Health Monitoring: A Review (2015, methodology): “” Michaels and Michaels [169] proposed damage detection in aluminum plates using an image fusion technique and Ng and Veidt [184], among several others, carried out damage localization in composite laminates.”
Assessment of delay-and-sum algorithms for damage detection in aluminium and composite plates (2014, methodology): “The residual signals from all the actuator-sensor paths are then shifted according to an appropriate time shifting rule and then summed to yield an average signal (Michaels and Michaels 2007).”