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Magnetic bearings for a spaceflight optical disk recorderThe development and testing of a magnetic bearing system for the translator of the read/write head in a magneto-optic disk drive are discussed. The asymmetrical three-pole actuators with permanent magnet bias support the optical head, and its tracking and focusing servos, through their radial excursion above the disk. The specifications for the magnetic bearing are presented, along with the configuration of the magnetic hardware. Development of a five degree of freedom collision model is examined which allowed assessment of the system response during large scale transients. Experimental findings and the results of performance testing are presented, including the roll-off of current-to-force due to eddy current loss in the magnetic materials.
Document ID
19910011882
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hockney, Richard
(SatCon Technology Corp. Cambridge, MA, United States)
Gondhalekar, Vijay
(SatCon Technology Corp. Cambridge, MA, United States)
Hawkey, Timothy
(SatCon Technology Corp. Cambridge, MA, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1991
Publication Information
Publication: NASA, Langley Research Center, Aerospace Applications of Magnetic Suspension Technology, Part 1
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91N21195
Funding Number(s)
CONTRACT_GRANT: NAS5-30309
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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