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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Mathematical modeling of a VSCF aircraft generating system


    Additional title:

    Mathematische Modelluntersuchung eines VSCF-Stromerzeugungssystems fuer Flugzeuge


    Contributors:
    Vadher, V.V. (author) / Smith, I.R. (author) / Williams, S. (author)

    Published in:

    Publication date :

    1986


    Size :

    10 Seiten, 9 Quellen



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    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