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NASA NTRS · 20150003318

Compact Active Vibration Control System for a Flexible Panel

Abstract

A diamond-shaped actuator for a flexible panel has an inter-digitated electrode (IDE) and a piezoelectric wafer portion positioned therebetween. The IDE and/or the wafer portion are diamond-shaped. Point sensors are positioned with respect to the actuator and measure vibration. The actuator generates and transmits a cancelling force to the panel in response to an output signal from a controller, which is calculated using a signal describing the vibration. A method for controlling vibration in a flexible panel includes connecting a diamond-shaped actuator to the flexible panel, and then connecting a point sensor to each actuator. Vibration is measured via the point sensor. The controller calculates a proportional output voltage signal from the measured vibration, and transmits the output signal to the actuator to substantially cancel the vibration in proximity to each actuator.

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BibTeXRIS

Schiller, Noah H., Cabell, Randolph H., Perey, Daniel F.. 2014-06-24. Compact Active Vibration Control System for a Flexible Panel. https://ntrs.nasa.gov/citations/20150003318

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