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Vibration attenuation using magnetic suspension isolationThe paper derives the vibration transfer function for a magnetic suspension in generic form, with specific reference to the Annular Suspension and Pointing System for Shuttle payloads. It is shown that a magnetically suspended pointer can exhibit considerably improved dynamic stability over conventional means, particularly at high frequencies and for transient disturbances. The amount of improvement to be anticipated is quantified to allow first-cut assessments for specific applications.
Document ID
19820029602
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Hamilton, B. J.
(Sperry Corp. Sperry Flight Systems, Phoenix, AZ, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1981
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: In: Joint Automatic Control Conference
Location: Charlottesville, VA
Start Date: June 17, 1981
End Date: June 19, 1981
Accession Number
82A13137
Funding Number(s)
CONTRACT_GRANT: NAS1-15008
Distribution Limits
Public
Copyright
Other

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