2015 IEEE International Symposium on Inertial Sensors and Systems (ISISS) Proceedings 2015
DOI: 10.1109/isiss.2015.7102360
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Disk resonator gyroscope with whole-angle mode operation

Abstract: We present a demonstration of a whole-angle mode operation of a 0.6 mm single-crystal silicon disk resonator gyroscope (DRG). This device has a Q factor of ~80,000 and a resonant frequency of ~250 kHz and is fabricated in the epi-seal process. Discrete-time control algorithms for rate-integrating gyro operation were implemented based on Lynch's algorithm. Despite the fact that this DRG is over 5 orders of magnitude smaller than the 58 mm HRG, the device's error sources are shown to be accurately modeled by the… Show more

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Cited by 56 publications
(22 citation statements)
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“…Because the QMG's high Q-factor results in a low (125 mHz) open-loop rate-sensing bandwidth, force-rebalanced operation [33,34] was also characterized at each bias voltage. The closed-loop bandwidth, shown in figure 8(c), was increased to 40 Hz, although the rate table's bandwidth limited experiments to a maximum input rate frequency of 5 Hz.…”
Section: Scale Factor Measurementsmentioning
confidence: 99%
“…Because the QMG's high Q-factor results in a low (125 mHz) open-loop rate-sensing bandwidth, force-rebalanced operation [33,34] was also characterized at each bias voltage. The closed-loop bandwidth, shown in figure 8(c), was increased to 40 Hz, although the rate table's bandwidth limited experiments to a maximum input rate frequency of 5 Hz.…”
Section: Scale Factor Measurementsmentioning
confidence: 99%
“…In summary, the above methods can reduce both the threshold and ADB to some extent, but they cannot fundamentally solve the problem of precession angular-rate bias errors introduced by the structural asymmetry of the gyro. The threshold and ADB of RIG are essentially caused by the bias terms of the anisostiffness and anisodamping in the precession angular rate of RIG [14], so the threshold and ADB could be significantly reduced by eliminating the bias terms in real time. To completely eliminate precession angular-rate bias errors, this paper introduces a novel compensation method based on a Fourier series fitting combined with a multiple iteration technique.…”
Section: Introductionmentioning
confidence: 99%
“…10 In this method, the two superimposed modes are separated using the orthogonality of the eigenmodes, and each mode is controlled independently by two phase-locked loops. 3,[11][12][13][14] In order to construct this type of gyroscope, a degenerate resonator is required. Furthermore, this type of gyroscope can be used as a rate integrating gyroscope that directly measures the rotation angle by reading the phase difference between the two modes.…”
Section: Introductionmentioning
confidence: 99%
“…10 Rate integrating gyroscopes are not temperature dependent like FM gyroscopes, and the measurement bandwidth can be infinity enlarged. 3,[11][12][13][14] In order to construct this type of gyroscope, a degenerate resonator is required. However, actual MEMS resonators have a degree of processing error, so they are not strictly degenerated.…”
Section: Introductionmentioning
confidence: 99%