A flight test system for a flapping-wing aerial vehicle includes a host computer platform, a measurement mechanism, and a wind tunnel. The measurement mechanism is configured to mount a to-be-tested flapping-wing aerial vehicle prototype. The measurement mechanism includes an Euler angle controller, a flow angle controller, and a tripod. The flow angle controller is mounted on the tripod. The Euler angle controller is in transmission connection with the flow angle controller. The flapping-wing aerial vehicle prototype is detachably connected to the Euler angle controller by using a first connecting member. The host computer platform is in communication connection with the measurement mechanism and the wind tunnel, and is configured to control a wind speed of the wind tunnel and display a flight status of the flapping-wing aerial vehicle prototype in real time during test.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Flight test system for flapping-wing aerial vehicle


    Beteiligte:
    HE WEI (Autor:in) / MU XINXING (Autor:in) / TIAN SHUFEN (Autor:in) / FU QIANG (Autor:in) / ZOU YAO (Autor:in) / HUANG HAIFENG (Autor:in) / HE XIUYU (Autor:in)

    Erscheinungsdatum :

    04.05.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



    FLAPPING WING AERIAL VEHICLE

    KARASEK MATEJ | Europäisches Patentamt | 2018

    Freier Zugriff

    FLAPPING WING AERIAL VEHICLE

    KARASEK MATEJ | Europäisches Patentamt | 2020

    Freier Zugriff

    FLAPPING WING AERIAL VEHICLE

    KARASEK MATEJ | Europäisches Patentamt | 2020

    Freier Zugriff

    Flapping wing micro-aerial-vehicle: Kinematics, membranes, and flapping mechanisms of ornithopter and insect flight

    Bin Abas, Mohd Firdaus / Bin Mohd Rafie, Azmin Shakrine / Bin Yusoff, Hamid et al. | British Library Online Contents | 2016


    Micro flapping-wing air vehicle with controllable wing flapping plane and flight control method of micro flapping-wing air vehicle

    WU JIANGHAO / SHENG SHIJIE / ZHANG YANLAI et al. | Europäisches Patentamt | 2024

    Freier Zugriff