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
2022-04-13
Patent
Elektronische Ressource
Englisch