The invention discloses a mother-son type unmanned aerial vehicle and a control method, the mother-son type unmanned aerial vehicle comprises a mother machine, the mother machine comprises a mother machine main body, a mother machine propeller and a driving assembly, and the mother machine main body is provided with a storage groove; the mother aircraft propeller is mounted on the mother aircraft main body; the driving assemblies are distributed on the two sides of the main machine body, the driving assemblies are connected with the main machine body in a turnover mode, and the driving assemblies can drive the main machine body to walk on the land when being turned over to the first position relative to the main machine body; and the son machine can be accommodated in the accommodating groove, is provided with a son machine propeller, and can fly away from the mother machine. The master aircraft adopts the configuration form of the variable-configuration air-ground amphibious unmanned aerial vehicle, different motion modes, namely, the flight mode and the land running mode, can be adopted according to different environments, and due to the fact that the electric quantity needed by the land running mode is smaller than that needed by the flight mode, energy can be saved, the operation time can be prolonged, and the unmanned aerial vehicle can adapt to more complex environments and is convenient to use. And the operation range is wider, and application scenes are more.

    本发明公开了一种子母式无人机及控制方法,子母式无人机包括:母机,包括:母机主体、母机螺旋桨和行驶组件,母机主体具有收纳槽;母机螺旋桨安装于母机主体;行驶组件分布于母机主体的两侧,且行驶组件与母机主体可翻转的连接,且行驶组件相对于母机主体翻转至第一位置时能够带动母机主体在陆地行走;子机,能够收纳于收纳槽内,且子机具有子机螺旋桨,且子机能够飞离所述母机。母机采用了可变构型的陆空两栖无人机的构型形态,可根据环境的不同,采用不同的运动模式,即飞行模式和陆地行驶模式,由于陆地行驶模式所需的电量小于飞行模式所需的电量,可节省能量,延长作业时间,并且能适应更复杂的环境,作业范围更广泛,应用场景更多。


    Access

    Download


    Export, share and cite



    Title :

    Primary-secondary type unmanned aerial vehicle and control method


    Additional title:

    一种子母式无人机及控制方法


    Contributors:
    ZHANG WANGWANG (author) / XU BIN (author) / FAN WEI (author) / LIU CHUNTAO (author)

    Publication date :

    2024-10-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Primary-secondary type unmanned aerial vehicle

    JIA YUSONG / SHEN YANG | European Patent Office | 2023

    Free access

    Primary-secondary separable unmanned aerial vehicle

    PENG JIE / JIANG WUGUI / ZHU MINJIAN et al. | European Patent Office | 2023

    Free access

    Split type unmanned aerial vehicle, unmanned aerial vehicle control system and control method

    ZHU HE / NIE HONG / DU YUHAO et al. | European Patent Office | 2023

    Free access

    Primary-secondary type unmanned aerial vehicle capable of automatically recovering and releasing secondary aircrafts

    YAN ZHIPING / HUA YUANYUAN / QU NIANMENG et al. | European Patent Office | 2022

    Free access

    Primary-secondary unmanned aerial vehicle with remote control signal relay device

    LI YUJIAO / ZHENG BINYAN / HUANG JIAQI et al. | European Patent Office | 2023

    Free access