DC/DC Converter for the International Space Station

被引：15

作者：

Belloni, Federico ^{[1
]}

Maranesi, Piero G. ^{[1
]}

Riva, Marco ^{[1
]}

机构：

[1] Univ Milan, Dept Phys, I-20133 Milan, Italy

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2010年 / 46卷 / 02期

关键词：

Switches; Aerodynamics; Voltage control; Power generation; DC-DC power converters; Load modeling;

D O I：

10.1109/TAES.2010.5461645

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A dc/dc converter for power distribution aboard the International Space Station (ISS) and space vehicles employing the 120 V dc bus is proposed. It is well suited to supply power to multiple loads including peripheral low voltage point-of-load (POL) regulators. The dc/dc converter is phase-shift controlled at the constant frequency of 500 kHz. The topology is characterized by distribution in a sequence of 4 metal-oxide semiconductor field-effect transistors (MOSFETs), switched ON at zero voltage. The linear model has first-order dynamics. Responses to small and large load variations benefit from its advantageous control features. A peculiar characteristic is its high dynamic independence of load typology and output power. To focus on this quality, dynamic performances are investigated through analyses, simulations, and measurements considering three types of loads: constant current, resistive, and constant power. Experimental data from a 100 W prototype fit the model forecasts well.

引用

页码：623 / 634

页数：12

共 23 条

[1] From the editors [J].

Bell, E ;

Honey, K ;

Minton, K ;

Bird, L .

NATURE REVIEWS IMMUNOLOGY, 2006, 6 (01) :1-1

[2] Experimental apparatus for testing the DC/DC converter dynamics [J].

Belloni, F. ;

Maranesi, P. G. ;

Riva, M. .

2007 IEEE POWER ELECTRONICS SPECIALISTS CONFERENCE, VOLS 1-6, 2007, :2498-2502

[3]

BELLOSA F, 2003, P WORKSH COMP OP SYS, P1

[4]

DALAL DB, 1990, APPL POWER ELECT CO, P265, DOI 10.1109/APEC.1990.66419

[5] A new digital control algorithm to achieve optimal dynamic performance in DC-to-DC converters [J].

Feng, Guang ;

Meyer, Eric ;

Liu, Yan-Fei .

IEEE TRANSACTIONS ON POWER ELECTRONICS, 2007, 22 (04) :1489-1498

[6] Current status, architecture, and future technologies for the International Space Station Electric Power System [J].

Gholdston, E ;

Hartung, J ;

Friefeld, J .

IEEE AEROSPACE AND ELECTRONIC SYSTEMS MAGAZINE, 1996, 11 (02) :25-30

[7]

Gietl EB, 2000, AEROSP CONF PROC, P47, DOI 10.1109/AERO.2000.878364

[8]

Hague LM, 1996, PROC IECEC, P154, DOI 10.1109/IECEC.1996.552863

[9]

Hart DS, 1997, IECEC-97 - PROCEEDINGS OF THE THIRTY-SECOND INTERSOCIETY ENERGY CONVERSION ENGINEERING CONFERENCE, VOLS 1-4, P280, DOI 10.1109/IECEC.1997.659199

[10]

HE Y, 2004, P IEEE 35 ANN POW EL, V1, P618

← 1 2 3 →