Disclosed is an aircraft attitude controller configured to obtain information representative of an attitude of an aircraft and, on the basis of the information, control the attitude of the aircraft by actively controlling a position of a winglet at a distal end of a wing portion of a wing of the aircraft, relative to the wing portion, thereby to control an angle of incidence of the winglet.


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    Titel :

    AIRCRAFT ATTITUDE CONTROLLER AND WING SYSTEM


    Weitere Titelangaben:

    FLUGZEUGLAGESTEUERUNG UND FLÜGELSYSTEM
    CONTRÔLEUR D'ATTITUDE D'AÉRONEF ET SYSTÈME D'AILE


    Beteiligte:

    Erscheinungsdatum :

    28.02.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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