MODELING AND SIMULATION OF SPACECRAFT POWER-SYSTEMS

被引:33
作者
LEE, JR
CHO, BH
KIM, SJ
LEE, FC
机构
[1] Virginia Polytechnic Inst &, State Univ, Blacksburg, VA, USA, Virginia Polytechnic Inst & State Univ, Blacksburg, VA, USA
关键词
ELECTRIC POWER SYSTEMS - Computer Simulation;
D O I
10.1109/7.192097
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Modeling of a complete spacecraft power processing system is presented, using the Boeing EASYS software. Component models are developed, and several system models including a solar array switching system, a partially shunted solar system, and cosmic background explorer (COBE) system are simulated. The modes of operation of the power system, such as shunt mode, battery-charge mode, and battery-discharge mode, are simulated for a complete orbit cycle.
引用
收藏
页码:295 / 304
页数:10
相关论文
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[2]  
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[3]  
CHO BH, 1985, 1985 IEEE POW EL SPE
[4]  
DECKER DK, 1981, 16TH IECEC ATL
[5]  
Kimble Stewart G., 1971, 1971 IEEE Power Electronics Specialists Conference, P77, DOI 10.1109/PESC.1971.7069137
[6]  
LEE JR, 1987, NASAGSFC1987 VIRG PO
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NEKRASOV PS, 1968, 14TH P ANN M AER AST
[8]  
ZIMMERMAN HG, 1970, IECEC 1970
[9]  
EASY5 DYNAMICS ANAL