The invention discloses a method and an aircraft capable of adaptively adjusting a focus position in flight. The aircraft comprises an aircraft body, wherein a main wing I and a main wing II which are positioned on two sides of the aircraft body, the aircraft body is provided with a load, a top end of the aircraft body is provided with symmetrically arranged empennages, empennage control surfaces matched with the empennages are arranged on the empennages, and translation mechanisms or rotating mechanisms correspondingly connected with the first main wing and the second main wing are symmetrically arranged in the aircraft body. According to flight control of the aircraft, the position relation of the gravity center and the focus is judged through empennage control surface deflection, then the position of the main wing is adjusted through the translation mechanism or the rotating mechanism to adjust the focus position of the aircraft, the flight gravity center and the focus are located at reasonable and safe positions, and deflection of the empennage control surface is reduced; and the aircraft is in a safe flight state and high in flight efficiency.

    本发明公开了一种可在飞行中自适应调节焦点位置的方法及飞行器,该飞行器包括机体和位于所述机体两侧的主翼一和主翼二,其特征在于,所述机体上设有负载,所述机体的顶端设有对称设置的尾翼,所述尾翼上均设有与其相匹配的尾翼舵面,所述机体内对称设有分别与所述主翼一和所述主翼二相对应连接的平移机构或旋转机构。本发明中飞行器飞控通过尾翼舵面偏转判断重心同焦点的位置关系,后通过平移机构或旋转机构来调整主翼位置从而达到调整飞行器焦点位置,使飞行重心与焦点处于合理安全位置,减少尾翼舵面的偏转,使飞行器处于安全飞行状态且飞行效率高。


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    Title :

    Method capable of adaptively adjusting focus position in flight and aircraft


    Additional title:

    一种可在飞行中自适应调节焦点位置的方法及飞行器


    Contributors:
    WANG ZHUO (author)

    Publication date :

    2021-08-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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