发明名称 Flexure Plate Capacitive Compass
摘要 A compass system includes a platform defining an x-axis, a y-axis and an xy-plane, wherein a z-axis is orthogonal to the xz-plane. A beam is rotatably coupled to the platform such that the beam rotates about the y-axis. An accelerometer including a flexure plate perpendicular to the y-axis is coupled to the beam a distance from the y-axis. The accelerometer generates an accelerometer signal in response to movement of the flexure plate. An angular position sensor senses angular position of the beam relative to the x-axis and y-axis, the angular position sensor generating an angular position signal therefrom. A processor receives the accelerometer signal and the angular position signal and generates an East-West signal therefrom.
申请公布号 US2005028392(A1) 申请公布日期 2005.02.10
申请号 US20030604624 申请日期 2003.08.05
申请人 THE BOEING COMPANY 发明人 CAMPBELL RAY F.;WADA JOAN D.
分类号 G01C19/38;(IPC1-7):G01C19/36 主分类号 G01C19/38
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