Disclosed is a computer-implemented method of determining a steering angle of an aircraft landing gear. The method comprises: obtaining an input image of the aircraft landing gear; comparing the input image against a plurality of reference images, the plurality of reference images comprising images of the aircraft landing gear at known steering angles; determining a most similar reference image, the most similar reference image comprising the reference image of the plurality of reference images most closely matched to the input image; and determining, based at least in part on the most similar reference image, the steering angle of the aircraft landing gear.
AIRCRAFT STEERING ANGLE DETERMINATION
BESTIMMUNG DES LENKWINKELS EINES FLUGZEUGES
DÉTERMINATION D'ANGLE DE BRAQUAGE D'UN AÉRONEF
2023-08-30
Patent
Elektronische Ressource
Englisch