DocumentCode :
321519
Title :
Power sizing and power performance simulation tools for general EPS analyses
Author :
Bailey, Patrick G. ; Lovgren, Jack
Author_Institution :
Lockheed Martin Missiles & Space, Sunnyvale, CA, USA
Volume :
1
fYear :
1997
fDate :
27 Jul-1 Aug 1997
Firstpage :
262
Abstract :
Several electric power system (EPS) modeling and simulation tools have been developed at Lockheed Martin that are being used in detailed EPS component designs and also in detailed EPS transient performance analyses. A consistent set of very detailed EPS components are used within each of the tools. The components can be chosen by the user to be very simple, such as time-averaged component values, or extremely detailed, such as instantaneous nonlinear models that have been verified against component test data. These tools have been used for a variety of satellite mission studies, and have been successfully used in both EPS component sizing studies and in detailed component and system transient performance calculations. Several EPS systems models are presented for discussion, the EPS component models are summarized in detail, and example results are included
Keywords :
artificial satellites; digital simulation; power system analysis computing; power system transients; space vehicle power plants; Lockheed Martin; component test data; electric power system modeling; instantaneous nonlinear models; power performance simulation tools; power sizing tools; satellite mission studies; system transient performance calculations; time-averaged component values; transient performance analyses; Analytical models; Batteries; Missiles; Orbital calculations; Performance analysis; Power system modeling; Power system simulation; Power system transients; Sun; Temperature;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Energy Conversion Engineering Conference, 1997. IECEC-97., Proceedings of the 32nd Intersociety
Conference_Location :
Honolulu, HI
Print_ISBN :
0-7803-4515-0
Type :
conf
DOI :
10.1109/IECEC.1997.659196
Filename :
659196
Link To Document :
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