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A passive pendulum wobble damper for a low spin rate Jupiter flyby spacecraftWhen the spacecraft has a low spin rate and precise pointing requirements, the wobble angle must be damped in a time period equivalent to a very few wobble cycles. The design, analysis, and test of a passive pendulum wobble damper are described.
Document ID
19720018747
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fowler, R. C.
(TRW Systems Group Redondo Beach, CA, United States)
Date Acquired
August 6, 2013
Publication Date
June 1, 1972
Publication Information
Publication: NASA. Ames Res. Center 6th Aerospace Mech. Symp.
Subject Category
Navigation
Accession Number
72N26397
Funding Number(s)
CONTRACT_GRANT: NAS2-5600
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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