Battery Discharge Regulator for Space Applications based on the Boost Converter

被引：12

作者：

Fernandez, A. ^{[1
]}

Tonicello, F. ^{[1
]}

Aroca, J. ^{[1
]}

Mourra, O. ^{[1
]}

机构：

[1] European Space Agcy, Energy & Power Convers Div, NL-2201 AZ Noordwijk, Netherlands

来源：

2010 TWENTY-FIFTH ANNUAL IEEE APPLIED POWER ELECTRONICS CONFERENCE AND EXPOSITION (APEC) | 2010年

关键词：

D O I：

10.1109/APEC.2010.5433476

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

When a DC/DC converter is used to control the power on the main bus of a spacecraft it needs to comply with highly demanding requirements from the dynamic point of view. Hence, converters with very good dynamic performance, i.e. with no zero on the right-half plane are typically used. The conventional boost converter has not been used in European space applications mainly because of its poor dynamics. This paper addresses the way of using a boost converter in this application and demonstrates that this converter can cope with the very demanding requirements needed. A prototype has been built and tested to proof it.

引用

页码：1792 / 1799

页数：8

共 13 条

[1]

[Anonymous], 2008, ECSSEST20C

[2]

COOKE P, IEEE PESC 2000, P256

[3]

Dixon LH., 1990, UN POW SUPPL DES SEM

[4]

Erickson R. W., 1997, Fundamentals of Power Electronics

[5]

LEE FC, 1991, VPEC POWER ELECT PRO

[6]

MIDDLEBROOK RD, 1985, IEEE PESC P JUN

[7]

OSULLIVAN D, IEEE PESC 88, P351

[8] Time-varying effects and averaging issues in models for current-made control [J].

Perreault, DJ ;

Verghese, GC .

IEEE TRANSACTIONS ON POWER ELECTRONICS, 1997, 12 (03) :453-461

[9]

Ridley R. B., 1989, PCIM '89 USA. Official Proceedings of the Nineteenth International Power Conversion (PCI) Conference, P455

[10]

Ridley R. B., 1990, Ph.D. dissertation

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