The invention discloses a novel unmanned aerial vehicle parameter debugging platform and debugging method. The novel unmanned aerial vehicle parameter debugging platform is composed of an aluminum profile body, a sliding rod structure, a ball head structure, a sliding block guide rail structure and a laser range finder. The debugging frame body is formed by building transverse and vertical external standard aluminum profiles and four inclined aluminum profiles, the aluminum profiles are combined and fixed through 45-degree inclined corner pieces and aluminum corner connectors, the sliding rod and the cylindrical sliding block are connected with the debugging frame body through the fixed carbon plate, the sliding rod is sleeved with the cylindrical sliding block, and therefore the unmanned aerial vehicle has the Z-axis freedom degree on the debugging frame. The upper ball head is connected with the debugging frame body through the supporting circular truncated cone, and the unmanned aerial vehicle is installed on the debugging frame through the aircraft installation disc. The linear sliding block drives the whole debugging frame body to move along the guide rail, the ball head is rotated by 90 degrees, and the X-axis freedom degree and the Y-axis freedom degree can be provided for the unmanned aerial vehicle at the same time. The debugging frame can meet the freedom degree of the X axis, the Y axis and the Z axis of the unmanned aerial vehicle and the rotation freedom degree of the unmanned aerial vehicle, and parameter debugging work is completed on the premise that the safety of unmanned aerial vehicle equipment is guaranteed.

    本发明公开了一种新型无人机参数调试平台及调试方法,由铝型材主体,滑杆结构,球头结构,滑块导轨结构和激光测距仪组成。调试架主体由横竖外标准铝型材外加四根斜铝型材搭建而成,铝型材之间由45°斜边角件和铝角码组合固定,滑杆和圆柱滑块与调试架主体之间经由固定碳板连接,滑杆套在圆柱滑块中,使得无人机在调试架上有Z轴的自由度。上方球头与调试架主体由支撑圆台相连,并通过飞行器安装盘将无人机安装在调试架上。直线滑块带动整个调试架主体沿导轨移动,将球头旋转90°,可同时为无人机提供X轴、Y轴自由度。本发明调试架可满足无人机X、Y、Z三轴的自由度和无人机自身旋转自由度,在保证无人机设备安全前提下完成参数调试工作。


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    Title :

    Novel unmanned aerial vehicle parameter debugging platform and debugging method


    Additional title:

    一种新型无人机参数调试平台及调试方法


    Contributors:
    SHEN YUE (author) / SUN HAO (author) / SHEN YAYUN (author) / YE HUASHENG (author) / WANG JIAJUN (author) / ZHANG YU (author) / HUANG YI (author)

    Publication date :

    2023-04-07


    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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