The invention relates to determining an aircraft steering angle. A computer-implemented method of determining a steering angle of an aircraft landing gear is disclosed. The computer-implemented method includes: acquiring a set of position data points, where the set of position data points includes position data points of a component of an aircraft landing gear; and calculating a centroid of the set of position data points. The method further includes determining an angle of intersection between: a straight line passing through both the center of mass and an axis of rotation of the aircraft landing gear; and an axis orthogonal to a strut of the aircraft landing gear with the aircraft landing gear at a previously known steering angle; and determining a steering angle of the aircraft landing gear based on the determined intersection angle.

    本发明涉及确定飞行器转向角度。公开了确定飞行器起落架的转向角度的计算机实现的方法。该计算机实现的方法包括:获取位置数据点的集合,其中,位置数据点的集合包括飞行器起落架的部件的位置数据点;以及计算位置数据点的集合的质心。该方法还包括确定以下两者之间的相交角度:穿过质心和飞行器起落架的旋转轴线两者的直线;以及在飞行器起落架处于预先已知的转向角度的情况下与飞行器起落架的支杆正交的轴线;以及基于所确定的相交角度来确定飞行器起落架的转向角度。


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    Titel :

    Determining aircraft steering angle


    Weitere Titelangaben:

    确定飞行器转向角度


    Beteiligte:
    OU DINGYU (Autor:in)

    Erscheinungsdatum :

    02.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01B MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS , Messen der Länge, der Dicke oder ähnlicher linearer Abmessungen / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS



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