Disclosed is a method of determining a steering angle of an aircraft landing gear. The method comprises: obtaining an image of the aircraft landing gear; performing edge detection on the image; determining, based at least in part on an edge obtained by the edge detection, a relative position of a component of the aircraft landing gear; and determining, based at least in part on the relative position of the component, the steering angle of the aircraft landing gear.
Aircraft steering angle determination
13.04.2022
Patent
Elektronische Ressource
Englisch