A modular state-variable approach is presented for DC spacecraft power system modeling and simulation. Each modular component is treated as a multiport network, and a state model is written with the port voltages as the inputs. The state model of a component is solved independently of the other components, using its state transition matrix. The state variables of each component are updated, assuming that the inputs are constant. Network analysis principles are then utilized to calculate the component inputs.


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    Titel :

    Simulation of DC spacecraft power systems


    Weitere Titelangaben:

    Simulation einer Gleichstrom-Versorgung fuer Raumfahrzeuge


    Beteiligte:
    Nelms, R.M. (Autor:in) / Grigsby, L.L. (Autor:in)


    Erscheinungsdatum :

    1989


    Format / Umfang :

    6 Seiten, 7 Quellen



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Simulation of AC spacecraft power systems

    Nelms, R.M. / Evans, B.W. / Grigsby, L.L. | Tema Archiv | 1989


    Simulation of DC spacecraft power systems

    Nelms, R.M. / Grigsby, L.L. | IEEE | 1989


    Modeling and simulation of spacecraft power systems

    Lee, J.R. / Cho, B.H. / Kim, S.J. et al. | Tema Archiv | 1988


    Modeling and Simulation of Spacecraft Power Systems

    Lee, J. R. / Cho, B. H. / Kim, S. J. et al. | AIAA | 1987


    Modeling and simulation of spacecraft power systems

    Lee, J.R. / Cho, B.H. / Kim, S.J. et al. | IEEE | 1988