The invention provides an aircraft anti-skid failure brake control method which comprises the steps that the working mode of a current anti-skid brake system of an aircraft is detected, and the working mode comprises a system normal working mode and an anti-skid failure brake control mode; if the current working mode of the anti-skid brake system of the airplane is an anti-skid failure brake control mode, adopted protection measures are determined, the protection measures comprise an amplitude limiting mode, a pulse adjusting mode and an amplitude limiting and pulse adjusting mode, and the protection measures comprise a corresponding relation between a brake instruction L determined by utilizing a preset coefficient K and output brake pressure P, wherein L belongs to [0, 1]; and according to the determined protection measures, brake control is conducted on the aircraft anti-skid brake system.

    本申请提供一种飞机防滑失效刹车控制方法,所述方法包括:检测飞机当前的防滑刹车系统的工作方式,所述工作方式包括系统正常工作模式和防滑失效刹车控制模式;若飞机当前的防滑刹车系统的工作方式为防滑失效刹车控制模式,则确定采用的保护措施,所述保护措施包括限幅方式、脉冲调节方式和限幅+脉冲调节方式,所述保护措施包括利用预设系数K确定的刹车指令L和输出刹车压力P的对应关系,所述L∈[0,1];根据确定的保护措施,对飞机防滑刹车系统进行刹车控制。


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    Titel :

    Aircraft anti-skid failure brake control method


    Weitere Titelangaben:

    一种飞机防滑失效刹车控制方法


    Beteiligte:
    LIU ZEHUA (Autor:in)

    Erscheinungsdatum :

    09.04.2021


    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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