Research of Battery Fault-Simulation on Primary Electrical Power System

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Abstract:

Battery, as one of the important parts in satellite electrical power system, is of a high probability of failure, therefore it is especially important to simulate and analysis. Base on the existing satellite power system simulation platform, this paper analysis on the fault of Low Earth Orbit (LEO) satellites lithium-ion (Li-Ion) battery. Storage battery, battery charge regulator (BCR) and battery discharge regulator (BDR) are modeled and simulated, and the models are built in Matlab/Simulink. The simulation results are realistic, and these models are effective methods for power design and fault recovery.

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Periodical:

Advanced Materials Research (Volumes 354-355)

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1174-1178

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October 2011

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© 2012 Trans Tech Publications Ltd. All Rights Reserved

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[1] P. G. Bailey, J. Lovgren, "Power Sizing and Power Performance Simulation Tools For General EPS Mission Analyses," 2nd International Energy Conversion Engineering Conference. Providence, Rhode Island. Angust 2004.

DOI: 10.2514/6.2004-5537

Google Scholar

[2] J.R. Lee, B.H. Cho, S.J. Kim, "Modeling and Simulation of Spacecraft Power Systems," IEEE Transactions on Aerospace and Electronic Systems, Vol. 24, 1998, pp.295-304.

DOI: 10.1109/7.192097

Google Scholar

[3] A. Patil, D. W. Shin, J. Choi, S. Yoon, "Structural and compositional characteristics of nanocrystalline nichrome thin film as anode for lithium battery,"Nanotechnology Materials and Devices Conference, 2006. IEEE Vol. 1, 2006, p.706 – 707.

DOI: 10.1109/nmdc.2006.4388971

Google Scholar

[4] M. Chen; G. A. Rincon-Mora, "Accurate, Compact, and Power-Efficient Li-Ion Battery Charger Circuit,"Circuits and Systems II: Express Briefs, IEEE Transactions on Vol. 53, 2006 , pp: 1180 – 1184.

DOI: 10.1109/tcsii.2006.883220

Google Scholar

[5] A.Fernandez, F.Tonicello, J. Aroca, O. Mourra, "Battery discharge regulator for space applications based on the boost converter," Applied Power Electronics Conference and Exposition (APEC), 2010 Twenty-Fifth Annual IEEE Digital Object Identifier , 2010, pp: 1792 – 1799.

DOI: 10.1109/apec.2010.5433476

Google Scholar

[6] L. Gao, S. Liu, R. A. Dougal, "Dynamic lithium-ion battery model for system simulation ,"Components and Packaging Technologies, IEEE Transactions on , Vol. 25, 2002, pp.495-505.

DOI: 10.1109/tcapt.2002.803653

Google Scholar

[7] G. Li, "Introduction to spacecraft power system technology".Beijing: China Aerospace Press, 2008, pp.131-132.

Google Scholar

[8] W. Zhang, "Modeling and Control of Switching Converters,"Beijing: China Electric Power Press, 2006, pp.7-9.

Google Scholar