EASYS modeling of a complete spacecraft power processing system is presented. Component models are developed, and several system models including a solar array switching system, a partially-shunted solar array system and COBE system are simulated. The power system's modes of operation, such as shunt mode, battery-charge mode, and battery-discharge mode, are simulated for a complete orbit cycle.


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    Title :

    Modeling and simulation of spacecraft power systems


    Additional title:

    Modellierung und Simulation des Energieversorgungssystems eines Raumfahrzeuges


    Contributors:
    Lee, J.R. (author) / Chao, B.H. (author) / Kim, S.J. (author) / Lee, F.C. (author)


    Publication date :

    1987


    Size :

    7 Seiten, 32 Bilder, 9 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Modeling and simulation of spacecraft power systems

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


    Modeling and simulation of spacecraft power systems

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


    Modeling and Simulation of Spacecraft Power Systems

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