The embodiment of the invention discloses an aircraft control method and device based on a dual-redundancy bus and an aircraft, the aircraft comprises a rack, a machine core and a motion attitude adjusting mechanism, and the motion attitude adjusting mechanism comprises a first bus, a second bus, a flight control computer and a control unit. The yaw control unit, the pitching control unit, the roll control unit and the accelerator control unit of the control unit are all connected with the first bus and the second bus, so that when the flight control computer communicates with the control units through the first bus and fails, the flight control computer can be switched to communicate through the second bus in time, and the communication efficiency is improved. The communication can be ensured to be uninterrupted, and the flight safety is further ensured; besides, four control units are adopted in the embodiment to control the yaw attitude, the pitch attitude, the roll attitude and the accelerator motion respectively, the problem of single-point failure is avoided, when one control lever fails, the whole aircraft cannot be out of control, and the flight safety is further guaranteed.

    本发明实施例公开了一种基于双余度总线的飞行器操纵方法、装置及飞行器,飞行器包括机架、机芯和运动姿态调整机构,其中运动姿态调整机构包括第一总线、第二总线、飞控计算机以及操纵单元,其中操纵单元的偏航操纵单元、俯仰操纵单元、横滚操纵单元、油门操纵单元,均是与第一总线和第二总线连接,因此,当飞控计算机通过第一总线与各操纵单元进行通信且失效时,可以及时的切换至通过第二总线进行通信,能够保证通信不断线,进而保障飞行安全;此外,实施例中采用四个操纵单元分别控制偏航姿态、俯仰姿态、横滚姿态和油门运动,避免出现单点故障问题,当其中一个操纵杆失效,不会影响整个飞行器失控,进一步保障了飞行安全。


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    Titel :

    Aircraft control method and device based on dual-redundancy bus and aircraft


    Weitere Titelangaben:

    一种基于双余度总线的飞行器操纵方法、装置及飞行器


    Beteiligte:
    ZHOU SHUANGJIU (Autor:in) / LIU YITAO (Autor:in) / WANG WEIMIN (Autor:in)

    Erscheinungsdatum :

    2022-12-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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