A control method for controlling a yaw angle γz and a roll angle γx of a vertical take-off aircraft comprising at least two drive groups arranged in opposite side regions of the aircraft so as to be spaced apart from a fuselage of the aircraft is presented. Each drive group comprises at least one first drive unit. The first drive unit is arranged so as to be spaced apart from the fuselage to pivot about a pivot angle α into a horizontal flight position and a vertical flight position.


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    Title :

    СПОСОБ УПРАВЛЕНИЯ ДЛЯ УПРАВЛЕНИЯ УГЛОМ РЫСКАНИЯ И КРЕНА ВЕРТИКАЛЬНО СТАРТУЮЩЕГО ЛЕТАТЕЛЬНОГО АППАРАТА


    Publication date :

    2021-07-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge