A gas turbine engine control system is disclosed having a model and an observer that together can be used to adjust a command issued to the gas turbine engine or associated equipment to improve performance. In one form the control system includes a nominal model that is adjusted to real time conditions. The adjusted model is used with a Kalman filter and is ultimately used to determine a perturbation to a control signal. In one form the perturbation can be to a legacy controller.


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    Title :

    GAS TURBINE ENGINE PERFORMANCE SEEKING CONTROL


    Additional title:

    OPTIMIERTE STEUERUNG FÜR GASTURBINENMOTORLEISTUNG
    COMMANDE D'OPTIMISATION DE PERFORMANCE DE MOTEUR À TURBINE À GAZ


    Contributors:

    Publication date :

    2022-02-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / B64C AEROPLANES , Flugzeuge / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    GAS TURBINE ENGINE PERFORMANCE SEEKING CONTROL

    KHALID SYED JALALUDDIN | European Patent Office | 2018

    Free access

    Gas turbine engine performance seeking control

    KHALID SYED JALALUDDIN | European Patent Office | 2017

    Free access

    Development of gas turbine performance seeking logic

    Jordan, D. / Michael, G.J. | Tema Archive | 1978


    Dual Engine application of the Performance Seeking Control algorithm

    MUELLER, F. / NOBBS, S. / STEWART, J. | AIAA | 1993


    Dual Engine application of the Performance Seeking Control algorithm

    Mueller, F. D. / Nobbs, S. G. / Stewart, J. F. | NTRS | 1993