发明名称 Improvements relating to angular rate sensor devices
摘要 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 Sin 3theta/Cos 3theta (vibration mode pair providing degenerate carrier and response parameters.
申请公布号 GB0001775(D0) 申请公布日期 2000.03.22
申请号 GB20000001775 申请日期 2000.01.27
申请人 BRITISH AEROSPACE PUBLIC LIMITED COMPANY 发明人
分类号 B81B3/00;G01C19/56;G01C19/5684;G01P9/04;H01L29/84 主分类号 B81B3/00
代理机构 代理人
主权项
地址