The invention belongs to the field of flight control, and particularly relates to a synchronous control device and method for a motor-driven distributed flap actuation system. The device comprises a flap control handle used for giving a target angle of flap movement; the flap digital controller is connected with the flap control handle and the position sensors of the two flaps, calculates the difference between the received target angle and the real-time angles, fed back by the position sensors, of the two flaps, and sends the difference to the two servo controllers; the number of the servo controllers is two, and the two servo controllers are respectively connected with a driving motor and are used for calculating the rotating speed of the motor according to the difference value; and the two driving motors are used for respectively driving the two flaps to deflect according to the motor rotating speeds analyzed by the servo controller. The synchronous control problem of the double independent motors is effectively solved, and synchronous movement of the left flap and the right flap is achieved.

    本申请属于飞行控制领域,特别涉及一种电机驱动的分布式襟翼作动系统同步控制装置及方法。该装置包括:襟翼控制手柄,用于给出襟翼运动的目标角度;襟翼数字控制器,连接所述襟翼控制手柄及两个襟翼的位置传感器,对接收到的目标角度与位置传感器反馈的两个襟翼的实时角度,计算差值,将所述差值发送给两个伺服控制器;伺服控制器,包括两个,两个伺服控制器各自连接一个驱动电机,用于根据所述差值计算电机转速;驱动电机,包括两个,用于根据伺服控制器解析的电机转速分别驱动两个襟翼偏转。本申请有效解决了双独立电机的同步控制问题,实现了左右襟翼的同步运动。


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    Titel :

    Synchronous control device and method for distributed flap actuating system driven by motor


    Weitere Titelangaben:

    一种电机驱动的分布式襟翼作动系统同步控制装置及方法


    Beteiligte:
    ZHANG QI (Autor:in) / CHEN XI (Autor:in) / LI HE (Autor:in) / XU AMENG (Autor:in)

    Erscheinungsdatum :

    2024-03-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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