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A TREETOPS Simulation of the STABLE Microgravity Vibration Isolation SystemAs a research facility for microgravity science, the International Space Station (ISS) will be used for numerous experiments which require a quiescent acceleration environment across a broad spectrum of frequencies. For many micro-gravity science experiments, the ambient acceleration environment on ISS will significantly exceed desirable levels. The ubiquity of acceleration disturbance sources and the difficulty in characterization of these sources precludes source isolation, requiring, vibration isolation to attenuate the disturbances to an acceptable level at the experiment. To provide a more quiescent acceleration environment, a vibration isolation system named STABLE (Suppression of Transient Accelerations By LEvitation) was developed. STABLE was the first successful flight test of an active isolation device for micro-gravity science payloads and was flown on STS-73/USML-2 in October 1995. This report documents the development of the high fidelity, nonlinear, multibody simulation developed using TREETOPS which was used to design the control laws and define the expected performance of the STABLE isolation system.
Document ID
19990021252
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Nurre, G. S.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Whorton, M. S.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Kim, Y. K.
(Alabama Univ. Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1999
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA/TM-1999-209009
M-906
NAS 1.15:209009
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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