DocumentCode :
2542421
Title :
Power flow for spacecraft power systems
Author :
Halpin, S.M. ; Grigsby, L.L. ; Sheble, G.B. ; Nelms, R.M.
Author_Institution :
Dept. of Electr. Eng., Auburn Univ., AL, USA
fYear :
1989
fDate :
6-11 Aug 1989
Firstpage :
143
Abstract :
A 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 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
Keywords :
graph theory; load flow; matrix algebra; space vehicle power plants; Newton-Raphson power flow; linear graph theory; network modeling technique; spacecraft power systems; system-level admittance matrix; Admittance; Graph theory; Load flow; Power system modeling; Power systems; Power transmission lines; Propagation losses; Space vehicles; Transmission line matrix methods; Transmission line theory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Energy Conversion Engineering Conference, 1989. IECEC-89., Proceedings of the 24th Intersociety
Conference_Location :
Washington, DC
Type :
conf
DOI :
10.1109/IECEC.1989.74453
Filename :
74453
Link To Document :
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