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NASA NTRS · 20080005018

Microgyroscope with closed loop output

Abstract

A micro-gyroscope (10) having closed loop operation by a control voltage (V.sub.TY), that is demodulated by an output signal of the sense electrodes (S1, S2), providing Coriolis torque rebalance to prevent displacement of the micro-gyroscope (10) on the output axis (y-axis). The present invention provides wide-band, closed-loop operation for a micro-gyroscope (10) and allows the drive frequency to be closely tuned to a high Q sense axis resonance. A differential sense signal (S1-S2) is compensated and fed back by differentially changing the voltage on the drive electrodes to rebalance Coriolis torque. The feedback signal is demodulated in phase with the drive axis signal (K.sub..omega..crclbar..sub.x) to produce a measure of the Coriolis force.

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BibTeXRIS

Challoner, A. Dorian, Gutierrez, Roman C., Tang, Tony K., Cargille, Donald R.. 2002-03-26. Microgyroscope with closed loop output. https://ntrs.nasa.gov/citations/20080005018

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