A gas-turbine aero-engine speed-control system has been investigated on an analogue computer to determine the possibility of using a model reference adaptive control device to maintain constant dynamic behaviour of engine speed irrespective of altitude and aircraft forward speed.


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    Title :

    Design analysis of model reference adaptive control systems applied to a gasturbine aircraft engine


    Contributors:

    Published in:

    Proceedings of the IEE ; 115 , 3 ; 460-466


    Publication date :

    1968


    Size :

    7 Seiten, 6 Bilder, 3 Tabellen, 13 Quellen


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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