The invention relates to the technical field of aviation flight control, and provides a flight control device, a control system and an aircraft, the flight control device comprises a manipulator and a feedback mechanism, the feedback mechanism is connected with the manipulator, and the feedback mechanism generates corresponding action damping according to a stress load signal and outputs the action damping to the manipulator. The feedback mechanism can receive a real-time stress load signal of the aircraft control surface, generate corresponding action damping according to the stress load signal and output the action damping to the manipulator, so that a driver can sense the loaded state of the aircraft control surface in real time through the control force, borne by the manipulator, of the action damping generated by the feedback mechanism. Therefore, the stress of the operator of the driver and the stress of the control surface of the aircraft are kept synchronous, the control over the flight attitude of the aircraft by the driver is improved, and the flight of the aircraft can be controlled more accurately and safely.

    本发明涉及航空飞行控制技术领域,提供一种飞行操纵装置、操纵控制系统及飞行器,包括操纵器和反馈机构,反馈机构与操纵器连接,反馈机构根据受力载荷信号产生相应的动作阻尼输出至操纵器,通过在操纵器上设置反馈机构,反馈机构能够接收飞行器舵面的实时受力载荷信号,并根据受力载荷信号产生相应的动作阻尼输出至操纵器,使驾驶员通过操纵器受到的来自反馈机构产生的动作阻尼的操纵力感实时感知飞行器舵面的受载状态,从而保证驾驶员的操纵器与飞行器舵面的受力保持同步,提高驾驶员对飞行器飞行姿态的控制,能够更加精准、安全地控制飞行器飞行。


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    Title :

    Flight manipulation device, manipulation control system and aircraft


    Additional title:

    飞行操纵装置、操纵控制系统及飞行器


    Contributors:
    ZOU XIANGFU (author) / CHEN XIPING (author)

    Publication date :

    2024-04-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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