The invention relates to a flapping wing motion control method based on flapping wing propulsion, and belongs to the technical field of propulsion equipment. The flapping wing motion comprises three motions including reciprocating oscillation motion in the horizontal direction and the vertical direction and pitching motion around a flapping wing rotating shaft, and the motion frequencies of the three motions are kept consistent; and the flapping wing motion is the circumferential motion in a # imgabs0 # shape on the whole. On the basis of a traditional flapping wing motion mode, three-degree-of-freedom coupling oscillation motion in the horizontal direction, the vertical direction and the pitching rotation direction is introduced for the first time, so that energy in the horizontal direction can be grabbed and used for improving the propelling performance.

    本发明涉及一种基于扑翼推进的扑翼运动控制方法,属于推进设备的技术领域。本发明的扑翼运动包含有三个运动,包括沿着水平方向和垂直方向的往复振荡运动以及绕着扑翼旋转轴的俯仰运动,三个运动的运动频率保持一致;所述扑翼运动是整体做#imgabs0#形的周向运动。本发明在传统扑翼运动方式的基础上,首次引入包含水平方向、垂直方向以及俯仰旋转方向的三自由度耦合振荡运动,使水平方向的能量亦可被攫取,并用于提升推进性能。


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    Title :

    Flapping wing motion control method based on flapping wing propulsion


    Additional title:

    基于扑翼推进的扑翼运动控制方法


    Contributors:
    LI YONGCHENG (author) / ZHANG MINGHUI (author) / LI YINGHUA (author) / XIAO DONGLIN (author) / PAN ZIYING (author) / WANG XIAOQING (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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