The invention provides an attitude control test device for an unmanned aerial vehicle. The attitude control test device comprises a base, a joint with more than three degrees of freedom, a sliding rod, a joint with more than two degrees of freedom, a mounting module, an unmanned aerial vehicle module and a simulation software module, wherein the base is fixed on the ground or a work surface; the sliding rod is connected with the base through the joint with more than three degrees of freedom; the mounting module is connected with the sliding rod through the joint with more than two degrees of freedom; the unmanned aerial vehicle module is mounted on the mounting module, so that the unmanned aerial vehicle module has degrees of freedom for rotating around the X axis, the Y axis and the Z axis, and degrees of freedom for moving along the X axis, the Y axis and the Z axis, namely six degrees of freedom in space in total. Through the dynamic response of the running unmanned aerial vehicle on the attitude control test device, control strategies and relevant parameters are adjusted in real time, so that scientific research personnel and engineers can conveniently develop and debug flight control products of unmanned aerial vehicles; besides, debugging can be safely performed indoors, so that the level of difficulties in research and development of products of unmanned aerial vehicles is lowered, and the industry of the unmanned aerial vehicles is promoted to quickly develop.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Attitude control test device for unmanned aerial vehicle


    Beteiligte:
    WANG HONGYU (Autor:in) / WANG YINGCHUN (Autor:in) / TIAN ZUOHUA (Autor:in) / DIAO QIZHUO (Autor:in) / LIU LING (Autor:in) / ZHAO XUN (Autor:in) / ZHANG BAOMIN (Autor:in)

    Erscheinungsdatum :

    2016-01-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Unmanned aerial vehicle attitude adjusting device

    ZHANG LIJIAN / JIANG ZHIGUANG / SHANG YANG et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Attitude control system of unmanned aerial vehicle

    LIANG JIMIN / ZHAO GANG / WANG WEIJUN et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Attitude control test device with external frame, for unmanned aerial vehicle

    WANG HONGYU / WANG YINGCHUN / TIAN ZUOHUA et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    Attitude control test device for six-degree-of-freedom unmanned aerial vehicle

    WANG HONGYU / TIAN ZUOHUA / DIAO QIZHUO et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    Aerial unmanned aerial vehicle with variable attitude

    FEI JIANHAO | Europäisches Patentamt | 2023

    Freier Zugriff