US patent US12747031
Determining a position of a component of an aircraft landing gear assembly
Abstract
A computer-implemented method of determining a position of a component of an aircraft landing gear assembly. The method includes obtaining an image of the aircraft landing gear assembly; determining a region of interest within the image, the region of interest contains the component of the aircraft landing gear assembly; calculating a coordinate of a centroid of the bounding box and comparing the coordinate of the centroid to a corresponding predetermined threshold coordinate to determine the position of the component of the aircraft landing gear assembly.