Concept for a power system controller for large space electrical power systems
Louis F. Lollar, John R. Lanier, James R. Graves, George C. Marshall Space Flight Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981 - Computers - 11 pages
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25 kW Power 8086 CPU requires ADDRESS BUS autonomous EPS operation baseline best microprocessor available breadboard PSC Center Director's Discretionary chargers and 12 Controller for Large CPU requires approximately DATA BUS Director's Discretionary Fund Discretionary Fund task Electrical Power Systems enable autonomous EPS fail-operational Power System flowchart four P3 function breadboard version I/O operations I/O PC board I/O port instructions Intel interface kW Power Module large multi-kW space Large Space Electrical limited function breadboard limited number load LOGIC AND BUFFERS Marshall Space Flight memory milliseconds to sample MODULE EPS BREADBOARD multi-kW space Electrical NASA PERFORMING ORGANIZATION potential cost savings power and distribution Power Module Breadboard POWER MODULE EPS power processor subsystems Power System Controller PSC breadboard PSC concept PSC consists PSC software PSC to enable PSC was developed registers Santa Clara Space Electrical Power Space Flight Center space power systems subsystem parameters teletype utilizing microprocessor technology ZILOG