发明名称 MICROELECTROMECHANICAL RATE SENSOR
摘要 A high signal to noise ratio circuit and signal processing scheme described herein provides signal power above a noise floor such that high performance rate gyro operation can be achieved. The technology described herein exploits the combination of very low noise rate signal front end and a carrier frequency locked to a crystal filter's passband. A fixed single frequency and a sampled alternating current amplitude for conveyance of rate information is utilized.
申请公布号 US2015304741(A1) 申请公布日期 2015.10.22
申请号 US201414256329 申请日期 2014.04.18
申请人 ROSEMOUNT AEROSPACE, INC. 发明人 McCall Hiram
分类号 H04Q9/14 主分类号 H04Q9/14
代理机构 代理人
主权项 1. A navigational-grade rate sensor system comprising: a motor module, a carrier module, and a signal compensation module, wherein the motor module, the carrier module, and the signal compensation module are each in communication with a first circuit; a second circuit in signal communication with the first circuit, wherein the second circuit is configured to generate system outputs and provide feedback signals to the motor module, the carrier module, and the signal compensation module.
地址 Burnsville MN US