The invention discloses a comprehensive test platform for an unmanned aerial vehicle. The comprehensive test platform comprises an external base, an outer ring, an inner ring, a fixed bracket and a control device, wherein the fixed bracket is connected with an unmanned aerial vehicle, two ends of the fixed bracket are mounted in the inner ring through first rotating shafts, the two ends of the inner ring are mounted in the outer ring through second rotating shafts, the two ends of the outer ring are installed in the external base through third rotating shafts, the fixed bracket can rotate around the first rotating shafts, the inner ring can rotate around the second rotating shafts, the outer ring can rotate around the third rotating shafts, the first rotating shafts, the second rotating shafts and the third rotating shafts are in a three-axis orthogonal relation in space, the first rotating shaft, the second rotating shaft and the third rotating shaft are each provided with an angle sensor, and various angle sensor are electrically connected with a control device. Compared with the comprehensive test platform in the prior art, the comprehensive test platform of the invention has the advantages that the working performance of the unmanned aerial vehicle in a flying state can be tested in various simulation environments, and the rejection rate and the risk of the unmanned aerialvehicle in the testing process are reduced.

    本发明公开了一种无人机综合测试平台,包括外部底座、外环、内环和固定支架和控制装置,固定支架用于与无人机连接,固定支架的两端通过第一旋转轴安装在内环的内部,内环的两端通过第二旋转轴安装在外环的内部,外环的两端通过第三旋转轴安装在外部底座的内部,固定支架可绕第一旋转轴旋转,内环可绕第二旋转轴旋转,外环可绕第三旋转轴旋转,第一旋转轴、第二旋转轴和第三旋转轴在空间上成三轴正交关系;第一旋转轴、第二旋转轴上、第三旋转轴上均安装有角度传感器,每个角度传感器均与控制装置电连接。本发明和现有技术相比所具有的优点是:能够在各种模拟环境下对处于飞行状态的无人机进行工作性能测试,降低无人机测试时的报废率和风险性。


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    Title :

    Comprehensive test platform for unmanned aerial vehicle


    Additional title:

    无人机综合测试平台


    Contributors:
    HUANG XINSHEN (author) / LI HAO (author) / ZHANG ZHENKUN (author) / WU ZHENG (author) / ZHOU QI (author) / MO LIANGJUN (author) / LI BINGFENG (author) / WANG JINSHA (author) / FAN WENYAN (author) / LIANG MING (author)

    Publication date :

    2020-05-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    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



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