NASA NTRS · 19840048960
Dynamic characterization and microprocessor control of the NASA/UVA proof mass actuator
Abstract
The self-contained electromagnetic-reaction-type force-actuator system developed by NASA/UVA for the verification of spacecraft-structure vibration-control laws is characterized and demonstrated. The device is controlled by a dedicated microprocessor and has dynamic characteristics determined by Fourier analysis. Test data on a cantilevered beam are shown.
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Zimmerman, D. C., Inman, D. J., Horner, G. C.. 1984-01-01. Dynamic characterization and microprocessor control of the NASA/UVA proof mass actuator. https://ntrs.nasa.gov/citations/19840048960
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