A digital computer was used to control an augmented turbofan engine and its inlet on a supersonic fighter. A brief summary of the system configuration and performance provides the background for remarks on the development of the system. Throughout the program a free flowing interchange of ideas, design, and test data was maintained among three major contractors and three Government facilities, aiding in the integration process.Particular emphasis is placed on:The role of simulation in system development,Software development and configuration control,Adaptation of the propulsion control system to a series of test facilities.Based on the experience acquired in the successful completion of the program, conclusions relevant to future engine/airframe development are drawn -- digital electronic engine controls are practical and essential for the fully integrated aircraft of the future. In addition specific recommendations are made for simulation and data reduction facilities for future engine controls development programs.


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    Titel :

    Use of a Digital Computer in an Integrated Propulsion Control System


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Carlin, C.M. (Autor:in) / Hastings, W.J. (Autor:in)

    Kongress:

    Aerospace Engineering and Manufacturing Meeting ; 1976



    Erscheinungsdatum :

    1976-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Use of a digital computer in an integrated propulsion control system

    Carlin, C. / Hastings, W. | Tema Archiv | 1976


    Integrated Propulsion Control System Program

    Bentz, Charles E. / Zeller, John R. | SAE Technical Papers | 1973



    Propulsion Control Design For A STOVL Integrated Flight/Propulsion Control System

    Watts, S. R. / Larkin, L. J. / Hill, B. H. et al. | British Library Conference Proceedings | 1993


    Integrated Propulsion System

    Robey, H. / American Society of Naval Engineers | British Library Conference Proceedings | 1995