The invention relates to a horizontal stabilizer trim control system and method. The balancing control method for the horizontal stabilizer comprises the following steps of: determining a control instruction by a flight control computer based on flight data according to a flight control rate, and respectively transmitting main/standby channel control signals to a first channel computer of a first balancing channel and a second channel computer of a second balancing channel through a first bus, one of the first balancing channel and the second balancing channel is determined to be a main balancing channel, a control instruction is transmitted to a main channel computer through a first bus, and the main channel computer transmits the control instruction to a main balancing electronic controller through a second bus. The main balancing electronic controller transmits a control instruction to the main control module, and the main control module applies the control instruction to the actuator. According to the horizontal stabilizer balancing control method disclosed by the invention, double simultaneous channel balancing can be effectively prevented in various working modes.

    本公开涉及水平安定面配平控制系统和方法。一种水平安定面配平控制方法可包括:由飞控计算机基于飞行数据根据飞行控制率确定控制指令,通过第一总线分别向第一配平通道的第一通道计算机以及第二配平通道的第二通道计算机传送主/备通道控制信号,以将第一配平通道和第二配平通道中的一者确定为主用配平通道,通过第一总线向主用通道计算机传送控制指令,由主用通道计算机通过第二总线将控制指令传送给主用配平电子控制器,由主用配平电子控制器向主用控制模块传送控制指令,以及由主用控制模块将控制指令作用于作动器。根据本公开的水平安定面配平控制方法能够在各种工作模式下有效防止双同时通道配平发生。


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    Titel :

    Horizontal stabilizer balancing control system


    Weitere Titelangaben:

    水平安定面配平控制系统


    Beteiligte:
    WANG JIAQI (Autor:in) / GU ZHICHAO (Autor:in) / LU JING (Autor:in) / HONG QIAN (Autor:in)

    Erscheinungsdatum :

    18.06.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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