• DocumentCode
    835564
  • Title

    Simulation of DC spacecraft power systems

  • Author

    Nelms, R.M. ; Grigsby, L.L.

  • Author_Institution
    Dept. of Electr. Eng., Auburn Univ., AL, USA
  • Volume
    25
  • Issue
    1
  • fYear
    1989
  • fDate
    1/1/1989 12:00:00 AM
  • Firstpage
    90
  • Lastpage
    95
  • Abstract
    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
  • Keywords
    circuit analysis computing; digital simulation; multiport networks; space vehicle power plants; DC spacecraft power systems; modeling; modular state-variable approach; multiport network; network analysis; simulation; state model; state transition matrix; DC-DC power converters; Equations; Power system dynamics; Power system interconnection; Power system modeling; Power system simulation; Power system stability; Power system transients; Space vehicles; Voltage;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.18665
  • Filename
    18665
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=835564