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A digital computer simulation and study of a direct-energy-transfer power-conditioning systemA digital computer simulation technique, which can be used to study such composite power-conditioning systems, was applied to a spacecraft direct-energy-transfer power-processing system. The results obtained duplicate actual system performance with considerable accuracy. The validity of the approach and its usefulness in studying various aspects of system performance such as steady-state characteristics and transient responses to severely varying operating conditions are demonstrated experimentally.
Document ID
19750017550
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Burns, W. W., III
(Duke Univ. Greenbelt, MD, United States)
Owen, H. A., Jr.
(Duke Univ. Greenbelt, MD, United States)
Wilson, T. G.
(Duke Univ.)
Rodriguez, G. E.
(NASA Goddard Space Flight Center)
Paulkovich, J.
(NASA Goddard Space Flight Center)
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Computer Programming And Software
Report/Patent Number
NASA-TM-X-66859
Report Number: NASA-TM-X-66859
Accession Number
75N25622
Funding Number(s)
CONTRACT_GRANT: NGL-34-001-001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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