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All-purpose bidirectional four-quadrant controllerThe basic purpose of this paper is to provide some information regarding bidirectional four quadrant resonant power conversion and describe possible applications to aircraft electrical systems. As this technology has been developed sufficiently to demonstrate its feasibility, this is an appropriate time to evaluate the benefits of its application to aircraft electrical systems.
Document ID
19840002003
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hansen, I. G. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1983
Publication Information
Publication: Aircraft Elect. Secondary Power
Subject Category
Aircraft Propulsion And Power
Accession Number
84N10070
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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