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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    F100 Multivarible Control System Engine Models/Design Criteria


    Contributors:

    Publication date :

    1976


    Size :

    134 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    F100 multivarible control system engine models/design criteria

    Miller, R.J. / Hackney, R.D. | Tema Archive | 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