The steps involved in the derivation of a mathematical model of a variable-speed constant-frequency (VSCF) DC-link generating system for use onboard an aircraft are outlined. The equations are arranged in a form which is suitable for numerical solution on a digital computer and are developed from considerations of various subnetworks of the overall network. One principal advantage of the technique described is that it leads to a systematic assembly and solution of the system equations, and thus to a considerably reduced computing time. The results presented are for a proposed system, and indicate the detail of both the steady-state and the transient response which can be provided by the system. This allows a system design to be arrived at which will comply with the requirements of a given performance specification.


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    Titel :

    Mathematical modeling of a VSCF aircraft generating system


    Weitere Titelangaben:

    Mathematische Modelluntersuchung eines VSCF-Stromerzeugungssystems fuer Flugzeuge


    Beteiligte:
    Vadher, V.V. (Autor:in) / Smith, I.R. (Autor:in) / Williams, S. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1986


    Format / Umfang :

    10 Seiten, 9 Quellen



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Mathematical Modeling of a VSCF Aircraft Generating System

    Vadher, V. V. / Smith, I. R. / Williams, S. | IEEE | 1986


    Aircraft VSCF generator expert system

    Ho, T.-L. / Bayles, R.A. / Sieger, E.R. | IEEE | 1988


    Variable Speed Constant Frequency (VSCF) Aircraft Electrical Power

    Canfield, E. B. / Summerford, J. W. | SAE Technical Papers | 1977


    Packaging the VSCF System for an Aircraft Engine Environment

    Pollard, David D. / Krajci, Gary E. | SAE Technical Papers | 1981