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NASA NTRS · 19910055215

Active control test on the Mini-Mast

Abstract

A 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.

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BibTeXRIS

Montgomery, Raymond C., Ghosh, Dave. 1990-01-01. Active control test on the Mini-Mast. https://ntrs.nasa.gov/citations/19910055215

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