stable flight can be achieved without the need for a complicated throttle operation by a pilot even when part or all of control surfaces malfunction. A computation means (15) calculates a thrust control signal for controlling engine thrust and a deflection angle control signal for controlling control surfaces based on state information regarding an airframe, and an operation command signal from an operation end. An engine driving means (17) drives an engine based on the thrust control signal. A control surface moving means (16) moves the control surfaces based on the deflection angle control signal.


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    Titel :

    CONTROL SYSTEM OF AIRCRAFT, METHOD FOR CONTROLLING AIRCRAFT, AND AIRCRAFT


    Weitere Titelangaben:

    STEUERSYSTEM FÜR EIN FLUGZEUG, VERFAHREN ZUR STEUERUNG EINES FLUGZEUGS UND FLUGZEUG
    SYSTÈME DE COMMANDE POUR AÉRONEF, PROCÉDÉ DE COMMANDE D'AÉRONEF ET AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    18.03.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge





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