The invention belongs to an aircraft structure and a control method thereof, and provides a fixed-wing aircraft capable of realizing vertical take-off and landing and a control method thereof in order to solve the technical problems that high-speed flat flight and small boundary dimension cannot be considered at the same time and control is complex in an existing high-speed vertical take-off and landing aircraft. Comprising a fuselage, a plurality of control surfaces, a plurality of power devices and a plurality of wings. The plurality of power devices and the plurality of wings are installed on the fuselage, the power devices are located on the front sides of the wings, the rear end of each wing is provided with a landing part, and the plurality of control surfaces are correspondingly installed on the plurality of wings respectively. Through cooperation of all the components, the aircraft has the vertical take-off and landing capacity and the high-speed level flight capacity and is compact in size.

    本申请属于一种飞行器结构及其控制方法,针对现有高速垂直起降飞行器存在高速平飞和小外形尺寸无法兼顾,以及控制复杂的技术问题,提供一种可垂直起降的固定翼飞行器及其控制方法,包括机身、若干个控制舵面、若干个动力装置和若干个机翼。若干个动力装置和若干个机翼均安装在机身上,动力装置位于机翼前侧,各机翼的后端均安装有起落件,若干个控制舵面分别对应安装在若干个机翼上。通过各部件的配合,使本申请的飞行器兼具垂直起降、高速平飞能力,且体积紧凑。


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    Title :

    Fixed-wing aircraft capable of vertically taking off and landing and control method thereof


    Additional title:

    一种可垂直起降的固定翼飞行器及其控制方法


    Contributors:
    XIONG JUNHUI (author) / CHEN XINMIN (author) / WU ZHENGYUAN (author) / LU JIANAN (author)

    Publication date :

    2024-04-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge




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