发明名称 SYSTEMATIC DISK RESONATOR GYROSCOPE TUNING
摘要 <p>Tuning an axisymmetric resonator such as in a disc resonator gyroscope (DRG) is disclosed. Frequency tuning a DRG in a single step informed by a systematic physical model of the resonator structure, sensing and actuation elements, such as a finite element model, is provided. The sensitivity of selected trimming positions on the resonator to reducing asymmetry terms is determined via perturbations of the systematic model. As well, the dependence of the parameters of model transfer functions between actuation and sensing elements on resonator asymmetry are systematically determined. One or two measured transfer functions may then be analyzed according to the systematic model to fully determine the needed asymmetry correction components of the DRG. One or two of four groups of four electrostatic bias electrodes or four groups of four laser trimming locations for the DRG are utilized to correct the asymmetry components which can give rise to mistuning.</p>
申请公布号 WO2009152260(A1) 申请公布日期 2009.12.17
申请号 WO2009US46932 申请日期 2009.06.10
申请人 THE BOEING COMPANY;CHALLONER, A., DORIAN 发明人 CHALLONER, A., DORIAN
分类号 G01C19/56 主分类号 G01C19/56
代理机构 代理人
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