The invention provides a horizontal stabilizer balancing system of an aircraft, a control method thereof and the aircraft, and the method comprises the following steps: a first motor controller determines a first to-be-executed balancing rate instruction according to a main computer, a working state and a communication state of a first channel and a suppression signal sent by a second channel; the second motor controller determines a second to-be-executed balancing rate instruction according to the main computer, the working state and the communication state of the second channel and the suppression signal sent by the first channel; and the main computer determines an execution controller from the first motor controller and the second motor controller according to the type information of the first to-be-executed balancing rate instruction and the second to-be-executed balancing rate instruction, so that the execution controller drives an actuator according to the corresponding to-be-executed balancing rate instruction, and balancing of the horizontal stabilizer is achieved. According to the invention, the dual-channel balancing risk can be avoided.

    本申请提出一种飞行器的水平安定面配平系统、其控制方法以及飞行器,其中,第一电机控制器根据主计算机、第一通道的工作状态和通信状态以及第二通道发送的抑制信号确定第一待执行配平速率指令;第二电机控制器根据主计算机、第二通道的工作状态和通信状态以及第一通道发送的抑制信号确定第二待执行配平速率指令;主计算机根据第一待执行配平速率指令与第二待执行配平速率指令的类型信息从第一电机控制器与第二电机控制器中确定执行控制器,以使得执行控制器根据对应的待执行配平速率指令驱动作动器,实现水平安定面的配平。本申请能够避免双通道配平风险。


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    Titel :

    Horizontal stabilizer balancing system of aircraft, control method of horizontal stabilizer balancing system and aircraft


    Weitere Titelangaben:

    飞行器的水平安定面配平系统、其控制方法以及飞行器


    Beteiligte:
    GU ZHICHAO (Autor:in) / ZHANG CHONG (Autor:in) / HU XIAOLI (Autor:in) / LIU JI (Autor:in)

    Erscheinungsdatum :

    08.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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