MODEL OF MICROMECHANICAL GYROSCOPE DYNAMICS BASED ON RING RESONATOR IN ELASTIC SUSPENSION
St. Petersburg State University of Aerospace Instrumentation, Department of Aerospace Instruments of Orientation, Navigation and Stabilization; Professor; Head of Department
V. K. Ponomarev
St. Petersburg State University of Aerospace Instrumentation, Department of Aerospace Instruments of Orientation, Navigation and Stabilization;
A. I. Panferov
St. Petersburg State University of Aerospace Instrumentation, Department of Aerospace Instruments of Orientation, Navigation and Stabilization;
N. A. Ovchinnikova
St. Petersburg State University of Aerospace Instrumentation, Department of Aerospace Instruments of Orientation, Navigation and Stabilization; Assistent
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Abstract. A model of micromechanical gyroscope dynamics is presented. The model accounts for the effects of mass, elastic, dissipative, and Coriolis forces from the gyroscope suspension.
Keywords:
micromechanical gyroscope, ring resonator, elastic suspension, radial and tangential loadings