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.


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    Title :

    Aircraft steering angle determination


    Publication date :

    2022-04-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



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