The application relates to the technical field of
nondestructive testing, and discloses an aircraft defect identification method and
system based on
tensor decomposition and an attention mechanism. The aircraft defect identification method based on
tensor decomposition and the attention mechanism comprises the following steps: acquiring multi-
modal data of an aircraft; constructing the multi-
modal data into a four-order space-time-
modal tensor, and generating a dynamic graph
structure based on the modal features of the tensor; applying a mixed constraint when decomposing the four-order tensor to obtain a core tensor and a
factor matrix; extracting features through multi-scale
pooling, combining topological persistent homology and a gated attention mechanism to distribute weights, and realizing
feature fusion; identifying a defect type based on the fused features, and locating a defect area by using a
factor matrix gradient amplitude and a dynamic threshold. Through multi-
modal data fusion, dynamic
graph regularization constraint and mixed
tensor decomposition technology, the application improves the detection sensitivity and positioning accuracy of small defects on the surface of the aircraft, and enhances the physical
interpretability of features and the robustness of the
algorithm to complex working conditions.