The embodiment of the invention provides an aircraft, which is characterized by comprising an aircraft body, an aircraft main body and an aircraft body, the main wings are fixedly connected with the fuselage, and the main wings are used for providing lift force for the aircraft; the canards are arranged at the positions, close to the aircraft head, of the aircraft body and used for providing lift force for the aircraft; the multi-rotor assembly comprises a first rotor assembly and a second rotor assembly; wherein; the first rotor assembly is mechanically coupled with the main wing; the second rotor assembly is rotatably connected with the canard, and the second rotor assembly is configured to be capable of adjusting the tilting angle of the second rotor assembly relative to the canard and providing lift force and/or forward pull force for the aircraft.

    本申请实施例提供了一种飞行器,其特征在于,所述飞行器包括:机身;主机翼,与所述机身固定连接,所述主机翼用于为所述飞行器提供升力;鸭翼,设置于所述机身靠近机头的位置,用于为所述飞行器提供升力;多旋翼组件,所述多旋翼组件包括第一旋翼组件和第二旋翼组件;其中;所述第一旋翼组件与所述主机翼机械耦合;所述第二旋翼组件与所述鸭翼可转动连接,其中,所述第二旋翼组件被配置为能够调整自身相对所述鸭翼的倾转角度,为所述飞行器提供升力和/或向前的拉力。


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    Title :

    Aircraft, aircraft control method and device, and computer readable storage medium


    Additional title:

    飞行器、飞行器的控制方法及装置、计算机可读存储介质


    Contributors:

    Publication date :

    2024-04-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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