An aircraft flight control system and method are provided. The system provides a control module that receives inertial data, sensor data, and a target airspeed. The control module processes the received data with aircraft thrust and drag models to evaluate the aircraft energy state. Based on the aircraft energy state, the control module determines (i) a maximum predicted potential flight path "max PPFP", defined by a maximum thrust at the target airspeed, and (ii) an idle predicted potential flight path, "idle PPFP," defined by an idle thrust at the target airspeed. The control module generates display commands for a display system to display (i) the flight path angle, (ii) the max PPFP and (iii) the idle PPFP. In addition, the control module generates and displays a predicted flight path speed indicator (PFPS) when the FPA is above the max PPFP or below the idle PPFP.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AUTOMATIC FLIGHT CONTROL SYSTEMS AND METHODS


    Weitere Titelangaben:

    SYSTEMES ET METHODES DE COMMANDE DE VOL AUTOMATIQUE


    Beteiligte:
    WYATT IVAN SANDY (Autor:in) / MELENDEZ LUIS VENTURA (Autor:in) / KOENIG JOHN (Autor:in) / ENGELS JARY (Autor:in)

    Erscheinungsdatum :

    2019-03-11


    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




    Automatic flight control systems

    Sadraey, Mohammad H. | TIBKAT | 2020


    Automatic flight control systems

    McLean, D. | Tema Archiv | 1990


    Automatic Flight Control Systems

    T. Hajduk | NTIS | 1969


    Automatic flight control systems

    Sadraey, Mohammad H. | TIBKAT | 2020