BSAC Seminar: Circular Orbit Operating Mode for MEMS Gyroscopes

August 28, 2012

Mitchell H. Kline

Electrical Engineering and Computer Sciences, UC Berkeley
BSAC Graduate Student Researcher
August 28, 2012 | 12:00 to 12:30 | 540 Cory Hall, DOP Center Conference Room
Host: Bernhard Boser

We present a gyroscope operating mode that reduces bias errors and scale factor drift and allows whole angle read-out. The gyroscope proof mass orbits in a circle at its natural frequency. An outside observer rotating under the proof mass then perceives a frequency change. If the observer rotates in the same direction as the orbital spin, the perceived frequency decreases, and in the opposite direction, the frequency increases. The addition of a second gyroscope that spins in the opposite direction enables a differential measurement, reducing temperature sensitivity. The frequency difference is exactly the angular rate; thus, the phase difference is the whole angle. Rate bias errors due to mechanical quadrature and cross-axis damping are periodic on the current angle of the proof mass relative to the sensor frame and are hence averaged out over one cycle. A 3-theta dual ring gyroscope chip with integrated CMOS buffer electronics and an off-chip controller demonstrates the technique.

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Jonathan Candelaria
Dalene Schwartz Corey