发明名称 Micromachined angular rate sensor
摘要 <p>An angular rate sensor device (10) such as a micro-machined vibrating structure gyroscope, comprises a resonator (16), drive means (18), sensing means (20) and associated electronic control means. The resonator (16), drive means (18), sensing means (20) and control means are fabricated from a layer of crystalline silicon (12) having a �100� principal crystal plane. In order to make the resonator (16) operate in this type of material without degrading its performance, the resonator (16) is arranged to be operated by the drive and sensing means (18, 20) under the control of the electronic control means with a vibration mode pair having modal parameters, such as Young's Modulus, matched to provide a consistent resonator response. In particular, the resonator (16) is arranged to be operated with a Sin3θ/Cos3θvibration mode pair providing degenerate carrier and response parameters. <IMAGE></p>
申请公布号 EP1120630(A1) 申请公布日期 2001.08.01
申请号 EP20000300602 申请日期 2000.01.27
申请人 BRITISH AEROSPACE PUBLIC LIMITED COMPANY 发明人
分类号 G01C19/5684;(IPC1-7):G01C19/56 主分类号 G01C19/5684
代理机构 代理人
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