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IPACS Attitude Control Technology ConsiderationsLarger facilities or the Space Station and its evolutionary versions are considered for the control bandwidth which will evolve to lower values, probably in the 0.01 to 0.1 hertz range. An integrated power attitude control systems (IPACS) unit that incorporates conventional mechanical bearings to have a bandwidth of 4-10 hertz is expected. If the IPACS unit incorporates the advanced technology magnetic bearing, a bandwidth of 1.2 hertz is expected. It is found that for the Space Station or even the Space Platform, either of the above IPACS concepts are adequate.
Document ID
19840004170
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brandon, L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 12, 2013
Publication Date
December 1, 1983
Publication Information
Publication: NASA. Langley Research Center Integrated Flywheel Technol., 1983
Subject Category
Spacecraft Propulsion And Power
Accession Number
84N12238
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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