The study of an acceleration sensing fuel control system for gas turbine engines using a small analog computer is presented. The transfer function technique is utilized in simulating the system which permitted a study of the system performance using a minimum of computer components. An actual engine was run using an electrical analog of the control developed on the computer. A system stability map (plot of maximum stable proportional gain versus maximum stable integral gain) is presented comparing calculated, computer, and actual engine results. The advantages of using the analog computer for control system analysis are illustrated.


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    Title :

    Gas Turbine Engine Analog Simulation for Acceleration Sensing Fuel Control Studies


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Pre-1964 SAE Technical Papers ; 1906



    Publication date :

    1963-01-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English