The objective of the F100 multivariable Control research program is to extend the linear quadratic regulator (LQR) theory to develop a 'practical' control system that can operate a state-of-the-art gas turbine engine over its entire flight envelope. The engine selected for this program is a Pratt and Whitney Aircraft F100 afterburning turbofan. To determine the adequacy of the control synthesis effort, the resulting control logic will be incorporated into a digital computer/controller, which then will be used to control a F100 engine in an altitude test facility at NASA Lewis Research Center. The F100 engine computer simulations, the control criteria for defining the basic requirements of a F100 control system, and a brief evaluation of the resulting LQR engine control system are presented in this report.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    F100 Multivarible Control System Engine Models/Design Criteria


    Beteiligte:
    R. J. Miller (Autor:in) / R. D. Hackney (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    134 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    F100 multivarible control system engine models/design criteria

    Miller, R.J. / Hackney, R.D. | Tema Archiv | 1976


    The F100 Engine

    Lancaster, Lanny T.G. / Eshbach, Russel E. | SAE Technical Papers | 1980



    F15/F100 engine diagnostic system

    SPETH, R. / SCOTT, B. / ROMOSER, B. | AIAA | 1979