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Adaptive Control of Truss Structures for Gossamer SpacecraftNeural network-based adaptive control is considered for active control of a highly flexible truss structure which may be used to support solar sail membranes. The objective is to suppress unwanted vibrations in SAFE (Solar Array Flight Experiment) boom, a test-bed located at NASA. Compared to previous tests that restrained truss structures in planar motion, full three dimensional motions are tested. Experimental results illustrate the potential of adaptive control in compensating for nonlinear actuation and modeling error, and in rejecting external disturbances.
Document ID
20070032064
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Yang Bong-Jun
(Georgia Inst. of Tech. Atlanta, GA, United States)
Calise, anthony J.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Craig, James I.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Whorton, Mark S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2007
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 8th Gossamer Spacecraft Forum
Location: Honolulu, HI
Country: United States
Start Date: April 23, 2007
End Date: April 26, 2007
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAG8-1912
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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