A hybrid electric propulsion system (100) includes a gas turbine engine (20) having at least one compressor section (24) and at least one turbine section (28) operably coupled to a shaft. The hybrid electric propulsion system includes an electric motor (212A,212B) configured to augment rotational power of the shaft of the gas turbine engine. A controller (256) is operable to determine an estimate of hybrid electric propulsion system parameters based on a composite system model (302) and sensor data, determine a model predictive control state and a prediction based on the hybrid electric propulsion system parameters and the composite system model, determine a model predictive control optimization for a plurality of hybrid electric system control effectors (240) based on the model predictive control state and the prediction using a plurality of reduced-order partitions of the composite system model, and actuate the hybrid electric system control effectors based on the model predictive control optimization.


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    Title :

    ADAPTIVE MODEL PREDICTIVE CONTROL FOR HYBRID ELECTRIC PROPULSION


    Additional title:

    ADAPTIVE MODELLPRÄDIKTIVE STEUERUNG FÜR ELEKTRISCHEN HYBRIDANTRIEB
    COMMANDE PRÉDICTIVE DE MODÈLE ADAPTATIF POUR PROPULSION ÉLECTRIQUE HYBRIDE


    Contributors:

    Publication date :

    2023-05-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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