SELF-ADAPTING DC CONVERTER FOR SOLAR SPACECRAFT POWER SUPPLY

被引：40

作者：

BOEHRINGER, AF

机构：

[1] Institut für Elektrische Anlagen, Technische Hochschule, Stuttgart

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 1968年 / AES4卷 / 01期

关键词：

D O I：

10.1109/TAES.1968.5408938

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The voltage-current characteristic of solar cells that provide power for a spacecraft can vary over a wide range. For maximum power transfer from the solar cells to the battery system a power converter has to be designed that adjusts its input impedance to a value equal to the output impedance determined by the operating power characteristic of the solar cells. This paper discusses a circuit and calculations for a design to match this condition. The proposed power converter is simple, lightweight, and reliable and will be used in the Sunblazer satellite. Copyright © 1968 by The Institute of Electrical and Electronics Engineers, Inc.

引用

页码：102 / +

页数：1