The authors present a steady-state security analysis and simulation of spacecraft power systems. A power flow simulates systems measurements for a given operating condition. A state estimator uses these measurements to estimate the state of the system. Using the results of the state estimator as the base case solution, a contingency analysis is performed to determine the system security for a given set of contingencies. Corrective control is applied to alleviate any problems found in the contingency analysis. The algorithm applies to either a single-phase system or the positive-per-phase equivalent of a three-phase system.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Simulation, estimation, analysis, and control of spacecraft power systems


    Weitere Titelangaben:

    Simulation, Schaetzung, Analyse und Regelung von Energiesystemen in Raumfahrzeugen


    Beteiligte:
    Williamson, S.H. (Autor:in) / Sheble, G.B. (Autor:in)


    Erscheinungsdatum :

    1989


    Format / Umfang :

    4 Seiten, 4 Quellen




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Simulation of DC spacecraft power systems

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


    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. / Chao, B.H. / Kim, S.J. et al. | Tema Archiv | 1987


    Modeling and simulation of spacecraft power systems

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