Fuselage surface damage defect automatic detection method and system based on deep learning
A deep learning and automatic detection technology, applied in machine learning, image data processing, instruments, etc., can solve problems such as heavy workload, difficult detection, and large aircraft fuselage structure, so as to improve efficiency and accuracy, and reduce labor intensity , Improve the efficiency of inspection and maintenance
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Embodiment 1
[0041] An automatic detection method for surface damage defects of a fuselage based on deep learning, the method is as follows:
[0042] A. Establish a defect sample model: collect the defect sample data of the aircraft fuselage, and establish a defect sample model based on the defect sample data;
[0043] A1. Obtain the image data of the aircraft fuselage by shooting with the multi-angle camera combination shooting system, and obtain the three-dimensional model of the fuselage through the three-dimensional synthesis system of the fuselage; this embodiment uses the multi-angle camera combination shooting system to collect and shoot the aircraft body to obtain the aircraft body Body image data, through the fuselage 3D synthesis system according to the aircraft fuselage image data reorganization and fitting to obtain the fuselage 3D model (can also include the fuselage 2D unfolded model, the fuselage 2D unfolded model is the plane unfolded view of the fuselage 3D model ), the 3D...
Embodiment 2
[0047] Such as Figure 1 ~ Figure 4 As shown, a method for automatic detection of damage defects on the fuselage surface based on deep learning is characterized in that: the method is as follows:
[0048] A. Establish a defect sample model: collect the defect sample data of the aircraft fuselage, and establish a defect sample model based on the defect sample data;
[0049] A1, obtain the image data of the aircraft fuselage by shooting with a multi-angle camera combination shooting system, and obtain the three-dimensional model of the fuselage through the three-dimensional synthesis system of the fuselage; the method for obtaining the image data of the aircraft fuselage in step A1 is as follows:
[0050] The method of this embodiment comprises an aircraft hangar and an aircraft propulsion device, the aircraft hangar has a hangar door, and the multi-angle camera combination shooting system is arranged on the hangar door of the aircraft hangar, and the multi-angle camera combinat...
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