The invention discloses an aircraft braking control method and device, an aircraft and a storage medium. The method comprises the following steps: acquiring an aircraft pitch angle at the current moment; determining an acceleration threshold value corresponding to the aircraft pitch angle by adopting a preset pitch angle and acceleration mapping table; and controlling the airplane to brake according to the acceleration threshold value. According to the embodiment of the invention, the acceleration threshold of aircraft braking can be adjusted according to the real-time taxiing state of the aircraft, so that the aircraft braking is accurately controlled, the forward turning accident caused by overlarge acceleration in the aircraft braking process is avoided, and the flight safety is improved.

    本发明公开了一种飞机刹停控制方法、装置、飞机及存储介质。该方法包括:获取当前时刻的飞机俯仰角;采用预先设定的俯仰角与加速度映射表,确定所述飞机俯仰角对应的加速度阈值;根据所述加速度阈值,控制飞机刹停。本发明实施例可以根据飞机实时滑行状态,调整飞机刹停的加速度阈值,从而准确控制飞机刹车,避免飞机刹停过程中由于加速度过大导致的前翻事故,提高飞行安全性。


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    Titel :

    Aircraft braking control method and device, aircraft and storage medium


    Weitere Titelangaben:

    一种飞机刹停控制方法、装置、飞机及存储介质


    Beteiligte:
    YU LEI (Autor:in) / ZHANG XIAOWEI (Autor:in) / GONG CHENG (Autor:in)

    Erscheinungsdatum :

    02.04.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF / B64C AEROPLANES , Flugzeuge



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