The invention relates to a method for controlling an aircraft taxiing system, comprising the steps of: generating a traction command (Com) for controlling a motor of a wheel drive actuator; detecting whether an external braking command is generated, wherein the external braking command aims at controlling the airplane wheel to brake through the brake; if the external braking command is generated, generating a predetermined minimum command (Cmp) to control the motor such that the drive actuator exerts a predetermined minimum motor torque on the wheel during braking, the minimum motor torque being strictly positive; it is detected whether the speed of the aircraft becomes zero and, if so, the predetermined minimum command (Cmp) is prohibited such that the drive actuator applies a zero torque on the wheel.

    本发明涉及一种用于控制飞行器滑行系统的方法,包括以下步骤:生成用以控制机轮驱动致动器的电机的牵引命令(Com);检测是否生成了外部制动命令,所述外部制动命令旨在通过制动器控制机轮制动;如果生成了所述外部制动命令,则产生用以控制所述电动机的预定最小命令(Cmp),使得所述驱动致动器在制动期间在所述机轮上施加预定最小电动机转矩,所述最小电动机转矩严格为正;检测所述飞行器的速度是否变为零,并且如果是,则禁止所述预定最小命令(Cmp),使得所述驱动致动器在所述机轮上施加零转矩。


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    Title :

    Method for controlling aircraft taxiing system


    Additional title:

    用于控制飞行器滑行系统的方法


    Contributors:

    Publication date :

    2022-11-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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