发明名称 Angular and linear flexure plate accelerometer
摘要 An accelerometer system includes a rigid plate system coupled to an inertial platform. A first flexure plate defines a first flex axis and is adjacent to the rigid plate system a first distance from the spin axis. The first flexure plate generates a first frequency signal in response to acceleration of the first flexure plate. A second flexure plate defines a second flex axis and is adjacent to the rigid plate system a second distance from the spin axis. The second flexure plate generates a second frequency signal in response to acceleration of the second flexure plate. A controller including receives the first frequency signal and the second frequency signal and generates an angular acceleration signal from a difference of the first frequency signal and the second frequency signal. The controller also generates a linear acceleration signal in response to an average of the first frequency signal and the second frequency signal. The controller also controls a missile system in response to the first frequency signal and the second frequency signal.
申请公布号 US6895321(B2) 申请公布日期 2005.05.17
申请号 US20030604529 申请日期 2003.07.29
申请人 THE BOEING COMPANY 发明人 CAMPBELL RAY F.;WADA JOAN D.;RAAB JOHN P.
分类号 G01C19/00;G01P15/08;G01P15/097;G01P15/125;G01P15/18;G06F7/70;(IPC1-7):G01P15/125 主分类号 G01C19/00
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