Aircraft inner cabin crack segmentation method based on adaptive non-local feature fusion
A feature fusion and self-adaptive technology, applied in neural learning methods, image analysis, computer components, etc., can solve problems such as inability to judge the shape, size and position of cracks, excessive downsampling, and unsatisfactory crack edge prediction results , to achieve the effect that is conducive to accurate measurement
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[0053] In order to further explain the technical means and effects of the present invention to achieve the intended purpose of the invention, the method for crack segmentation of aircraft inner cabin based on adaptive non-local feature fusion proposed according to the present invention will be described in detail below in conjunction with the accompanying drawings and specific implementation methods .
[0054] The aforementioned and other technical contents, features and effects of the present invention can be clearly presented in the following detailed description of specific implementations with accompanying drawings. Through the description of specific embodiments, the technical means and effects of the present invention to achieve the intended purpose can be understood more deeply and specifically, but the accompanying drawings are only for reference and description, and are not used to explain the technical aspects of the present invention. program is limited.
[0055] I...
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