Disclosed is a computer-implemented method of determining a steering angle of an aircraft landing gear. The computer-implemented method comprises obtaining a set of position data points, wherein the set of position data points comprises position data points of a component of the aircraft landing gear and calculating a centroid of the set of position data points. The method also comprises determining an angle of an intersection between a straight line that passes through both the centroid and an axis of rotation of the aircraft landing gear and an axis that is orthogonal to a strut of the aircraft landing gear when the aircraft landing gear is at a previously known steering angle, and determining the steering angle of the aircraft landing gear based on the determined angle of intersection.


    Access

    Download


    Export, share and cite



    Title :

    Determining aircraft steering angle


    Publication date :

    2023-03-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



    Determining aircraft steering angle

    OU DINGYU | European Patent Office | 2024

    Free access

    Determining aircraft steering angle

    TING YU AU | European Patent Office | 2025

    Free access

    DETERMINING AIRCRAFT STEERING ANGLE

    AU TING YU | European Patent Office | 2024

    Free access

    DETERMINING AIRCRAFT STEERING ANGLE

    AU TING YU | European Patent Office | 2024

    Free access

    Aircraft steering angle determination

    ETHAN MOSS | European Patent Office | 2023

    Free access