The invention relates to a control method for controlling a yaw angle


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    Title :

    Control method for controlling a yaw angle and a roll angle of an aircraft that takes off vertically


    Contributors:

    Publication date :

    2024-06-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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