“…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 ].…”