A method and control system for controlling the thrust of an aircraft. A thrust request is input into a controller and the controller determines throttle, governor, and RPM setpoints to meet the input thrust request. The controller can determine minimum and maximum available thrust limits of the engine and can modify any of the setpoints if any setpoint violates the available thrust limit.


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    Title :

    DIRECT THRUST CONTROL METHOD FOR AIRCRAFT THRUSTER


    Additional title:

    DIREKTES SCHUBSTEUERUNGSVERFAHREN FÜR EIN FLUGZEUGTRIEBWERK
    PROCÉDÉ DE COMMANDE DE POUSSÉE DIRECTE POUR PROPULSEUR D'AÉRONEF


    Contributors:

    Publication date :

    2025-03-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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