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Mechanisms of the Space Active Vibration Isolation (SAVI)The Space Active Vibration Isolation (SAVI) is a concept for vibration isolation of one body from another with simultaneous precise control in 6 Degrees Of Freedom (DOF). SAVI achieves this using a combination of electromechanical linear actuators and magnetic actuators. Other mechanisms of interest include a structure for simulating the body being pointed, an apparatus to simulate the body that is the vibration source, and mechanisms to off-load the weight of each of these two bodies from the experiment to approximate a zero-g condition. A SAVI was built and tested to demonstrate these capabilities.
Document ID
19920015841
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schmitt, Frank
(Honeywell, Inc. Glendale, AZ, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1992
Publication Information
Publication: NASA. Goddard Space Flight Center, The 26th Aerospace Mechanisms Symposium
Subject Category
Structural Mechanics
Accession Number
92N25084
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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