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Concept for a power system controller for large space electrical power systemsThe development of technology for a fail-operatonal power system controller (PSC) utilizing microprocessor technology for managing the distribution and power processor subsystems of a large multi-kW space electrical power system is discussed. The specific functions which must be performed by the PSC, the best microprocessor available to do the job, and the feasibility, cost savings, and applications of a PSC were determined. A limited function breadboard version of a PSC was developed to demonstrate the concept and potential cost savings.
Document ID
19820003236
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Lollar, L. F.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Lanier, J. R., Jr.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Graves, J. R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1981
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TP-1939
Report Number: NASA-TP-1939
Accession Number
82N11109
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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