A flight control system for controlling an aircraft during a variable engine thrust takeoff operation operative to perform a method including calculating a calculated acceleration in response to a takeoff distance and a selection of a variable engine thrust takeoff mode, generating an initial thrust control signal in response to the calculated acceleration, controlling a thrust of an aircraft engine in response to the initial thrust control signal, measuring a measured acceleration of the aircraft, generating an updated thrust control signal in response to a difference between the calculated acceleration and the measured acceleration, and controlling the thrust of the aircraft engine in response to the updated thrust control signal.


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    Titel :

    CONTROLLERS AND AIRCRAFT WITH VARIABLE ENGINE THRUST TAKEOFF SYSTEM


    Weitere Titelangaben:

    REGLER UND FLUGZEUG MIT VARIABLEM MOTORSCHUBSTARTSYSTEM
    ORGANES DE COMMANDE ET AÉRONEF DOTÉ D'UN SYSTÈME DE DÉCOLLAGE À POUSSÉE MOTEUR VARIABLE


    Beteiligte:
    HORNE THOMAS C (Autor:in) / LANDERS THOMAS (Autor:in) / LAVRISA THOMAS P (Autor:in) / SWAINE SUZANNE (Autor:in)

    Erscheinungsdatum :

    2024-04-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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