The invention discloses a steering control method and system for a steering engine-driven flapping-wing air vehicle. The method comprises the following steps: receiving a steering control instruction; wherein the steering control instruction comprises first inclination angle information and first amplitude information; analyzing the steering control instruction to obtain a corresponding first inclination angle and a first amplitude; wherein the first wing is a left wing or a right wing of the ornithopter; according to the first inclination angle and the first amplitude, a first lower flapping angle and a first upper flapping angle are obtained through calculation; generating a first pulse width modulation signal according to the first lower flapping angle and the first upper flapping angle; and controlling a first wing to flap according to the first pulse width modulation signal. Steering control over the flapping-wing air vehicle can be achieved without depending on an empennage, and the steering flexibility of the flapping-wing air vehicle is improved.

    本发明公开了一种舵机驱动扑翼飞行器的转向控制方法及系统,其中方法包括:接收转向控制指令;其中,所述转向控制指令包括第一倾斜角信息与第一幅值信息;解析所述转向控制指令,得到对应的第一倾斜角与第一幅值;其中,所述第一翅翼为扑翼飞行器的左翼或右翼;根据所述第一倾斜角和第一幅值,计算得到第一下扑角和第一上扑角;根据所述第一下扑角和所述第一上扑角,生成第一脉冲宽度调制信号;根据所述第一脉冲宽度调制信号,控制第一翅翼扑动。本发明不依靠尾翼便可实现对扑翼飞行器的转向控制,提高了扑翼飞行器转向的灵活性。


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    Titel :

    Steering control method and system for flapping-wing air vehicle driven by steering engine


    Weitere Titelangaben:

    一种舵机驱动扑翼飞行器的转向控制方法及系统


    Beteiligte:
    SU LIANG (Autor:in) / LI KANGBAO (Autor:in) / YANG JINGJING (Autor:in) / ZHANG TONG (Autor:in) / YANG XIAONIU (Autor:in)

    Erscheinungsdatum :

    26.01.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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