The invention discloses a vertical take-off and landing unmanned aerial vehicle and a control method thereof, and relates to the field of unmanned aerial vehicles. The unmanned aerial vehicle comprises a tilting support, paired rotor wing supports, at least two rotor wings and a lifting wing, wherein the paired rotor wing supports are arranged at two ends of the tilting support respectively; the at least two rotor wings are divided into two groups, and each group of rotor wings are rotatably mounted on the paired rotor wing supports through rotor wing rotating shafts respectively; and the lifting wing is arranged on the tilting support, and the angles of the lifting wing relative to the rotor wing support planes where the paired rotor wing supports are located are adjustable. The unmannedaerial vehicle control method comprises the steps that in the cruising process, the angle between the lifting wing and the rotor wing support plane is adjusted, so that the rotor wing support plane and the lifting wing form a set angle under the condition that the lifting wing is kept basically horizontal. By controlling the tilting angle of the lifting wing, the dead weight of the unmanned aerialvehicle in the cruising state and in the take-off and landing process is reduced, and the technical problem that in the prior art, extra power consumption is too high is solved.

    本发明公开了一种垂直起降无人机及其控制方法,涉及无人机领域。该无人机包括倾转支架;成对的旋翼支架,分别设置在所述倾转支架的两端;至少两个旋翼,所述至少两个旋翼分为两组,每组所述旋翼分别通过旋翼转轴可旋转地安装在成对的旋翼支架上;和升力翼,设置在所述倾转支架上,并相对于所述成对的旋翼支架所在的旋翼支架平面角度可调。该无人机控制方法包括在巡航过程中,调整所述升力翼与所述旋翼支架平面的角度,以便在所述升力翼保持基本水平的条件下,使所述旋翼支架平面与所述升力翼呈设定角度。本发明通过控制升力翼的倾转角度,减少无人机在巡航状态及起降过程中的死重,解决了现有技术中普遍存在的额外功耗过高的技术问题。


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    Title :

    Vertical take-off and landing unmanned aerial vehicle and control method thereof


    Additional title:

    一种垂直起降无人机及其控制方法


    Contributors:
    WANG PENG (author)

    Publication date :

    2020-07-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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