In the feedback control design of multivariable systems, closed loop performance evaluations must include the dynamic behavior of variables unavailable to the feedback controller. For the multivariable Nyquist array method, a set of sensitivity functions are proposed to simplify the adjustment of compensator parameters when the dynamic response of the unmeasurable output variables is unacceptable. A sensitivity study to improve thrust and turbine temperature responses for the Pratt-Whitney F100 turbofan engine demonstrates the utility of the proposed method.


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    Titel :

    A sensitivity analysis for the F100 turbofan engine using the multivariable Nyquist array


    Beteiligte:

    Kongress:

    Modeling and simulation. Volume 9 - Ninth Annual Pittsburgh Conference ; 1978 ; Pittsburgh, PA


    Erscheinungsdatum :

    01.01.1978


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Multivariable control altitude demonstration on the F100 turbofan engine

    Lehtinen, B. / Dehoff, R. L. / Hackney, R. D. | NTRS | 1979


    Multivariable control altitude demonstration on the F100 turbofan engine

    Lehtinen, B. / Dehoff, R. L. / Hackney, R. D. | NTRS | 1979


    Multivariable control altitude demonstration on the F100 turbofan engine

    LEHTINEN, B. / DEHOFF, R. / HACKNEY, R. | AIAA | 1979



    Altitude calibration of an F100, S/N P680063, turbofan engine

    Biesiadny, T. J. / Lee, D. / Rodriguez, J. R. | NTRS | 1978