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Micromechanical gyroscope finite-element analysis
Mechanical analysis by method of finite-element analysis of the construction of two-component micromechanical gyroscope is explored. 3D geometric model and finite-element model of the gyroscope are made. Natural frequencies and mode shapes of the gyroscope are determined. Parameters ensuring resonan...
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Published in: | IEEE aerospace and electronic systems magazine 2008-09, Vol.23 (9), p.28-30 |
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container_title | IEEE aerospace and electronic systems magazine |
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creator | Nesterenko, T.G. Plotnikova, I.V. Plotnikov, I.A. Lysova, O.M. Zhaldybin, L.D. |
description | Mechanical analysis by method of finite-element analysis of the construction of two-component micromechanical gyroscope is explored. 3D geometric model and finite-element model of the gyroscope are made. Natural frequencies and mode shapes of the gyroscope are determined. Parameters ensuring resonance tuning are realized. The choice of the most appropriate variant of construction takes place by realizing of modal analysis and varing of sensor's geometry. Deformations of device construction elements determined at maximum of the measured velocity. |
doi_str_mv | 10.1109/MAES.2008.4635068 |
format | magazinearticle |
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subjects | Aircraft components Construction Electronic systems Finite element method Finite element methods Frequency Geometry Gyroscopes Mathematical analysis Mathematical models Micromechanical devices Modal analysis Resonance Shape Solid modeling Tuning |
title | Micromechanical gyroscope finite-element analysis |
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