A computer-implemented method of determining a steering angle of an aircraft landing gear is disclosed including 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 includes 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.


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    Title :

    DETERMINING AIRCRAFT STEERING ANGLE


    Contributors:
    AU TING YU (author)

    Publication date :

    2024-08-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01S RADIO DIRECTION-FINDING , Funkpeilung



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