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Voltage and Current Control for Spacecraft Fuel-Cell Systems

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1 Author(s)
Bills, Glenn W. ; Space and Information Systems Division North American Aviation, Inc. Downey, California

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.

Published in:

Aerospace, IEEE Transactions on  (Volume:2 ,  Issue: 2 )

Date of Publication:

April 1964

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