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Power flow for spacecraft power systemsA method for constructing the generalized system-level admittance matrix for use with a Newton-Raphson power flow is presented. The network modeling technique presented does not use the standard pi-equivalent models, which assume a lossless return path, for the transmission line and transformer. If the return path cannot be assumed lossless, then the standard algorithms for constructing the system admittance matrix cannot be used. The method presented here uses concepts from linear graph theory to combine network modules to form the system-level admittance matrix. The modeling technique is presented, and the resulting matrix is used with a standard Newton-Raphson power flow to calculate all system voltages and current (power) flows.
Document ID
19900050999
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Halpin, S. M.
(Auburn Univ. AL, United States)
Grigsby, L. L.
(Auburn Univ. AL, United States)
Sheble, G. B.
(Auburn Univ. AL, United States)
Nelms, R. M.
(Auburn University AL, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: IECEC-89
Location: Washington, DC
Country: United States
Start Date: August 6, 1989
End Date: August 11, 1989
Accession Number
90A38054
Funding Number(s)
CONTRACT_GRANT: NAGW-1192
Distribution Limits
Public
Copyright
Other

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