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Active control test on the Mini-MastA Linear Quadratic Gaussian (LQG) design process is presented and applied to a large flexible ground test facility, the Mini-Mast, for validation. For the design, nine displacement sensors were used. Three torque wheel actuators were used for damping augmentation. Results were dramatic, indicating an improvement in damping from 3 percent to 30 percent of critical. The tests proved the effectiveness of the procedure in designing effective vibration damping systems.
Document ID
19910055215
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Montgomery, Raymond C.
(NASA Langley Research Center Hampton, VA, United States)
Ghosh, Dave
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1990
Subject Category
Ground Support Systems And Facilities (Space)
Meeting Information
Meeting: NASA-UCLA Workshop on Computational Techniques in Identification and Control of Flexible Flight Structures
Location: Lake Arrowhead, CA
Country: United States
Start Date: November 2, 1989
End Date: November 4, 1989
Sponsors: University of California, ComCon Conference Board, NASA
Accession Number
91A39838
Distribution Limits
Public
Copyright
Other

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