1996 Solid-State, Actuators, and Microsystems Workshop Technical Digest 1996
DOI: 10.31438/trf.hh1996.65
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Silicon Bulk Micromachined Vibratory Gyroscope

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Cited by 28 publications
(11 citation statements)
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“…The excitations of the sensor's lightly damped modes can be accomplished by applying a potential to the driving electrodes directly from a function generator or digital-to-analog converter (DAC) and the subsequent response is measured by converting the charge on the sense electrodes into a buffered output voltage that is proportional to the rate of change of the gap between the electrodes and the cloverleaf. More detailed information on the design and fabrication of the sensors is provided in [18].…”
Section: A Sensor Descriptionmentioning
confidence: 99%
“…The excitations of the sensor's lightly damped modes can be accomplished by applying a potential to the driving electrodes directly from a function generator or digital-to-analog converter (DAC) and the subsequent response is measured by converting the charge on the sense electrodes into a buffered output voltage that is proportional to the rate of change of the gap between the electrodes and the cloverleaf. More detailed information on the design and fabrication of the sensors is provided in [18].…”
Section: A Sensor Descriptionmentioning
confidence: 99%
“…Inspection of (7) shows that the outputs are symmetric in the mistuning factor and that the sets G i Y i and G q Y q determine the dependence on the frequency parameter #. Figures 7 and 8 show Bode plots of G i and G q for a typical value of $ 2 and for dierent values of mistuning .…”
Section: Tuned Gyromentioning
confidence: 99%
“…Displacements in the negative z-axis direction are considered positive. The conversion factors from velocity t o v oltage for each electrode are denoted K S1 and K S2 and are used to de ne the scaling matrix K S as shown in (10). Thus, the gyroscope output equation is…”
Section: Computing Sti Ness Matrix Principal Axes From Input/output Modelsmentioning
confidence: 99%
“…Microgyroscopes will augment other external inertial reference systems such as the Global Positioning System (GPS), sun sensor, or star tracker in future planetary y-by and landing, and interplanetary astrophysics research programs, will use this technology. Tang et al (1996a) gives an overview of the role of micro-inertial systems in spacecraft. The summary by Y azdi et al (1998) describes other e orts to develop a MEMS gyroscope.…”
Section: Introductionmentioning
confidence: 99%