DocumentCode
2098420
Title
Bilateral power conditioner
Author
Cardwell, G.I. ; Neel, W. O., III
Author_Institution
Hughes Aircraft Company, El Segundo, California
fYear
1973
fDate
11-13 June 1973
Firstpage
214
Lastpage
221
Abstract
Modem high power spacecraft operating in near earth orbit require efficient switching regulation in both battery charge and discharge control. In the past, the charge and discharge functions have been performed by separate power conditioners with separate power inductors, power filter capacitors, as well as separate duty cycle control modulators. In an effort to reduce weight, complexity, cost, and improve efficiency, a unique bilateral power conditioner was conceived. This system effectively minimizes part count, weight, and complexity as well as increasing reliability by utilizing common filters and control circuits for both the charge and discharge functions. A description of the requirements, development, circuit operation, circuit comparisons, and performance of the system is presented in this paper.
Keywords
Batteries; Detectors; Discharges (electric); Modulation; Switches; Transistors; Voltage control;
fLanguage
English
Publisher
ieee
Conference_Titel
Power Electronics Specialists Conference, 1973 IEEE
Conference_Location
Pasadena, California, USA
ISSN
0275-9306
Type
conf
DOI
10.1109/PESC.1973.7065191
Filename
7065191
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