The invention provides a flight test system for a flapping-wing flying robot. The flight test system comprises an upper computer platform, a measuring mechanism and wind tunnel equipment, wherein themeasuring mechanism is used for installing a flapping-wing flying robot prototype to be measured, and the measuring mechanism and the flapping-wing flying robot prototype are arranged in wind tunnel equipment; the measuring mechanism comprises an attitude angle controller, an airflow angle controller and a triangular bracket, wherein the airflow angle controller is installed on the triangular support, the attitude angle controller is in transmission connection with the airflow angle controller, and the flapping wing flying robot prototype is detachably connected with the attitude angle controller through a first connecting piece; and the upper computer platform is in communication connection with the measuring mechanism and the wind tunnel equipment, and is used for controlling the wind speed of the wind tunnel equipment and displaying the flight state of the flapping-wing flying robot prototype in real time. According to the invention, the dynamic characteristics of the flapping-wingflying robot can be measured and analyzed, the flying performance can be tested, and the effect of verifying the model operation effectiveness can be achieved.

    本发明提供一种面向扑翼飞行机器人的飞行测试系统,其包括上位机平台、测量机构和风洞设备;其中,测量机构用于安装待测的扑翼飞行机器人样机,二者一同置于风洞设备中;测量机构包括姿态角控制器、气流角控制器和三角支架;其中,气流角控制器安装在三角支架上,姿态角控制器与气流角控制器传动连接,扑翼飞行机器人样机通过第一连接件与姿态角控制器可拆卸地连接;上位机平台与测量机构和风洞设备通信连接,用于在测试中控制风洞设备的风速并实时显示扑翼飞行机器人样机的飞行状态。本发明有助于测量和分析扑翼飞行机器人动力学特性,测试飞行性能,并可起到模型运行有效性验证的作用。


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    Titel :

    Flight test system for flapping-wing flying robot


    Weitere Titelangaben:

    一种面向扑翼飞行机器人的飞行测试系统


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

    Erscheinungsdatum :

    2020-06-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    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 / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen



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