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Spacecraft power system compatibility and stability for the NASA EOS satelliteThis paper addresses the problem of system stability of the NASA EOS satellite power system. A potential stability problem exists without a clear specification of the payload input impedance characteristic. Design guidelines are established for the control of the power system and the individual subcomponents to help insure stability with an unknown complex load. A testbed of the EOS power system is employed to verify the analysis.
Document ID
19930041863
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sable, Dan M. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Cho, Bo H. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Lee, Fred C. (Virginia Polytechnic Inst. and State Univ. Blacksburg, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: IECEC '92; Proceedings of the 27th Intersociety Energy Conversion Engineering Conference, San Diego, CA, Aug. 3-7, 1992. Vol. 1 (A93-25851 09-44)
Publisher: Society of Automotive Engineers, Inc.
Subject Category
Spacecraft Propulsion And Power
Accession Number
93A25860
Funding Number(s)
CONTRACT_GRANT: NAS5-31442
Distribution Limits
Public
Copyright
Other

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