DocumentCode
1229594
Title
Voltage and Current Control for Spacecraft Fuel-Cell Systems
Author
Bills, Glenn W.
Author_Institution
Space and Information Systems Division North American Aviation, Inc. Downey, California
Volume
2
Issue
2
fYear
1964
fDate
4/1/1964 12:00:00 AM
Firstpage
478
Lastpage
482
Abstract
This paper proposes a possible feedback control system for regulating the output voltage and currents of a spacecraft electric power system consisting of parallel fuel-cell modules. Such a control system may be necessary because of the many fuel cell variables that can change the value of the fuel-cell module terminal voltage and cause an unequal division of load between the modules.
Keywords
Aerospace control; Current control; Equations; Fuel cells; Impedance; Power system reliability; Space heating; Space vehicles; Temperature; Voltage control;
fLanguage
English
Journal_Title
Aerospace, IEEE Transactions on
Publisher
ieee
ISSN
0536-1516
Type
jour
DOI
10.1109/TA.1964.4319627
Filename
4319627
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