The need for a more sophisticated engine control system is discussed. The improvements in better thrust-to-weight ratios demand the manipulation of more control inputs. New technological solutions to the engine control problem are practiced. The digital electronic engine control (DEEC) system is a step in the evolution to digital electronic engine control. Technology issues are addressed to ensure a growth in confidence in sophisticated electronic controls for aircraft turbine engines. The need of a control system architecture which permits propulsion controls to be functionally integrated with other aircraft systems is established. Areas of technology studied include: (1) control design methodology; (2) improved modeling and simulation methods; and (3) implementation technologies. Objectives, results and future thrusts are summarized.


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    Titel :

    Control technology for future aircraft propulsion systems


    Beteiligte:
    Zeller, J. R. (Autor:in) / Szuch, J. R. (Autor:in) / Merrill, W. C. (Autor:in) / Lehtinen, B. (Autor:in) / Soeder, J. F. (Autor:in)


    Erscheinungsdatum :

    1984-03-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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