An aircraft includes an airframe having an aircraft longitudinal axis and a main rotor system supported by the airframe. The main rotor system is rotatable about an axis of rotation. The airframe is tiltable relative to a ground surface to form a non-zero tilt angle between the aircraft longitudinal axis and the ground surface.


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    Title :

    ENHANCED TAXI CONTROL FOR RIGID ROTORS


    Additional title:

    VERBESSERTE ROLLSTEUERUNG FÜR STARRE ROTOREN
    COMMANDE DE ROULAGE TAXI AMÉLIORÉE POUR DES ROTORS RIGIDES


    Contributors:

    Publication date :

    2021-03-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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