The invention provides a control system of an unmanned aerial vehicle capable of vertically taking off and landing. A fixed wing system and a vertical take-off and landing system are arranged on the unmanned aerial vehicle body at the same time, the unmanned aerial vehicle is controlled to operate in a vertical take-off and landing mode during take-off and landing, and take-off or landing is achieved through the vertical take-off and landing system; in the process that the unmanned aerial vehicle rises to a certain height and flies, the unmanned aerial vehicle is controlled to operate in a fixed wing mode, driving force is output through an obliquely-arranged fixed wing propelling device to drive the unmanned aerial vehicle to fly, and driving energy consumption is reduced. According to the unmanned aerial vehicle control system provided by the invention, various external devices can be conveniently carried, loaded and unloaded, the energy consumption required by flight is lower, and due to the arrangement of the vertical take-off and landing system, take-off and landing can be conveniently carried out in a small space.

    本发明提供一种可垂直起降的无人机的控制系统。本发明在无人机机身上同时设置固定翼系统和垂直起降系统,在起飞降落时控制无人机运行在垂直起降模式,通过垂直起降系统起飞或降落;在无人机上升到一定高度飞行的过程中,控制无人机运行在固定翼模式,通过倾斜设置的固定翼推进装置输出驱动力驱动无人机飞行,节省驱动能耗。本发明所提供的无人机控制系统,方便搭载装卸各类外接设备,飞行所需能耗更低,且由于垂直起降系统的设置,能够方便的在较小的空间内进行起降。


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    Titel :

    Control system of unmanned aerial vehicle capable of vertically taking off and landing


    Weitere Titelangaben:

    一种可垂直起降的无人机的控制系统


    Beteiligte:
    YAO DECHEN (Autor:in) / YANG JIANWEI (Autor:in) / SUN QIANG (Autor:in) / ZHANG JIAO (Autor:in) / WU XIANGPENG (Autor:in) / LIU HENGCHANG (Autor:in) / KOU ZIMING (Autor:in)

    Erscheinungsdatum :

    2020-05-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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