The control evaluated has been designed for the F100-PW-100 turbofan engine. The F100 engine represents the current state-of-the-art in aircraft gas turbine technology. The control makes use of a multivariable, linear quadratic regulator. The evaluation procedure employed utilized a real-time hybrid computer simulation of the F100 engine and an implementation of the control logic on the NASA LeRC digital computer/controller. The results of the evaluation indicated that the control logic and its implementation will be capable of controlling the engine throughout its operating range.


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    Title :

    Evaluation of an F100 multivariable control using a real-time engine simulation


    Contributors:
    Szuch, J. R. (author) / Soeder, J. F. (author) / Skira, C. (author)

    Conference:

    Propulsion Conference ; 1977 ; Orlando, FL, US


    Publication date :

    1977-07-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English