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Modeling and simulation of spacecraft power systemsEASY5 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.
Document ID
19880024659
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lee, J. R. (Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Cho, B. H. (Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Kim, S. J. (Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Lee, F. C. (Virginia Polytechnic Institute and State University Blacksburg, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: IECEC ''87
Location: Philadelphia, PA
Country: United States
Start Date: August 10, 1987
End Date: August 14, 1987
Accession Number
88A11886
Funding Number(s)
CONTRACT_GRANT: NAG5-518
Distribution Limits
Public
Copyright
Other

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