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Advanced actuators for the control of large space structuresThe objective of this research was to develop advanced six-degree-of-freedom actuators employing magnetic suspensions suitable for the control of structural vibrations in large space structures. The advanced actuators consist of a magnetically suspended mass that has three-degrees-of-freedom in both translation and rotation. The most promising of these actuators featured a rotating suspended mass providing structural control torques in a manner similar to a control moment gyro (CMG). These actuators employ large-angle-magnetic suspensions that allow gimballing of the suspended mass without mechanical gimbals. Design definitions and sizing algorithms for these CMG type as well as angular reaction mass actuators based on multi-degree-of-freedom magnetic suspensions were developed. The performance of these actuators was analytically compared with conventional reaction mass actuators for a simple space structure model.
Document ID
19930018383
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Downer, James
(SatCon Technology Corp. Cambridge, MA, United States)
Hockney, Richard
(SatCon Technology Corp. Cambridge, MA, United States)
Johnson, Bruce
(SatCon Technology Corp. Cambridge, MA, United States)
Misovec, Kathleen
(SatCon Technology Corp. Cambridge, MA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Publication Information
Publication: NASA. Langley Research Center, Magnetic Suspension Technology Workshop
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93N27572
Funding Number(s)
CONTRACT_GRANT: NAS1-18426
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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