The invention relates to the technical field of unmanned aerial vehicle yaw angle correction, and discloses an unmanned aerial vehicle oblique photogrammetry yaw angle automatic correction mechanism which comprises a main body mechanism and a control mechanism, the control mechanism is located below the main body mechanism, and the main body mechanism comprises an unmanned aerial vehicle main body, a wing frame and supporting legs. The wing frame is fixedly mounted at the outer end of the unmanned aerial vehicle main body, and the supporting legs are fixedly mounted at the lower end of the unmanned aerial vehicle main body; the main body mechanism further comprises a photographing host, a camera, an inclination angle horizontal sensor and a fixing plate. According to the automatic deviation rectifying mechanism for oblique photogrammetry of the yaw angle of the unmanned aerial vehicle and the use method thereof, the automatic deviation rectifying assembly is installed, so that the unmanned aerial vehicle can automatically rectify the angle of a video recorder, and the unmanned aerial vehicle can adjust the appropriate yaw angle for shooting; the problem that later picture splicing is difficult due to the flight deflection angle during oblique photography of an existing unmanned aerial vehicle is effectively solved, the practicability is higher during use, and use is more flexible.

    本发明涉及无人机偏航角纠偏技术领域,且公开了一种无人机倾斜摄影测量偏航角自动纠偏机构,包括主体机构和控制机构,所述控制机构位于主体机构的下方,所述主体机构包括无人机主机体、机翼架和支撑脚,所述机翼架固定安装在无人机主机体的外端,所述支撑脚固定安装在无人机主机体的下端;所述主体机构还包括摄影主机、摄像头、倾角水平传感器、固定板。该无人机倾斜摄影测量偏航角自动纠偏机构及其使用方法,通过安装自纠偏组件,便于使得该无人机能够实现自动纠偏录像机角度使其调节合适的偏航角进行拍摄,有效解决了现有无人机倾斜摄影时由于航偏角问题导致后期拼接画面较困难的问题,在使用时的实用性更强,使用时更加灵活。


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    Titel :

    Automatic deviation correcting mechanism for oblique photogrammetry yaw angle of unmanned aerial vehicle and use method of automatic deviation correcting mechanism


    Weitere Titelangaben:

    一种无人机倾斜摄影测量偏航角自动纠偏机构及其使用方法


    Beteiligte:
    WANG YAN (Autor:in) / ZHANG KANGKANG (Autor:in) / SUN SHENG (Autor:in) / WU JIAJIA (Autor:in) / CHEN ZE (Autor:in) / CHANG HAODONG (Autor:in) / WEN JUAN (Autor:in) / GU JINJIN (Autor:in) / CHEN MENGYAO (Autor:in) / WANG YUTING (Autor:in)

    Erscheinungsdatum :

    2023-07-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U



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