The purpose of the present invention is to provide a flight control mechanism for controlling flight of an unmanned aerial vehicle by controlling collision between the vehicle and a boundary surface, an unmanned aerial vehicle equipped with the mechanism, and a method for using the mechanism and the vehicle. Provided is a flight control mechanism for an unmanned aerial vehicle including: a first initial collision member; a second initial collision member; and a holding member that holds the first and second initial collision members with a space therebetween above the body of the unmanned aerial vehicle, is tiltable with respect to the vehicle body by rotating about a predetermined position inside or above the vehicle body toward the side of the vehicle body, and rotates in response to collision between the first or second initial collision member and a boundary surface.


    Access

    Download


    Export, share and cite



    Title :

    Unmanned Aerial Vehicle, Flight Control Mechanism for Unmanned Aerial Vehicle, and Method for Using Unmanned Aerial Vehicle and Mechanism for Unmanned Aerial Vehicle


    Contributors:

    Publication date :

    2021-05-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge






    Unmanned aerial vehicle wing limiting mechanism, unmanned aerial vehicle wing and unmanned aerial vehicle

    ZHANG KE / ZHANG XIAOPAN / ZHANG YING et al. | European Patent Office | 2023

    Free access

    Unmanned aerial vehicle arm mechanism and unmanned aerial vehicle

    WU SHAOQIANG / ZHANG LIANG / GUO XIHUA | European Patent Office | 2024

    Free access