The invention discloses a control method of an unmanned aerial vehicle capable of vertically taking off and landing. 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 a vertical take-off and landing system; in the process that the unmanned aerial vehicle rises to a certain height andflies, 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 method provided by the invention, the energy consumption required by flight is lower, and due tothe arrangement of the vertical take-off and landing system, take-off and landing can be conveniently carried out in a smaller space.
一种可垂直起降的无人机的控制方法。本发明控制无人机起飞降落时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方法,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。
Control method of unmanned aerial vehicle capable of vertically taking off and landing
一种可垂直起降的无人机的控制方法
2020-05-15
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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