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.


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    Titel :

    Aircraft steering angle determination


    Erscheinungsdatum :

    2022-04-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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