Title :
Voltage and Current Control for Spacecraft Fuel-Cell Systems
Author_Institution :
Space and Information Systems Division North American Aviation, Inc. Downey, California
fDate :
4/1/1964 12:00:00 AM
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;
Journal_Title :
Aerospace, IEEE Transactions on
DOI :
10.1109/TA.1964.4319627
