发明名称 INTEGRATED OPTICS GYROSCOPE SENSOR
摘要 INTEGRATED OPTICS GYROSCOPE SENSOR An integrated optical gyro sensor comprising a Sagnac interferometer, having a light source, a plurality of optical waveguides and an optical coupling arrangement integrated onto a substrate. The substrate has multiple light waveguides and detectors integrated therein. The primary waveguide has a roughly spiral shape with its respective ends disposed approximately 90 degrees to each other. The optical coupling arrange-ment comprises four beamsplitters and a reflector, which couple light signals to the primary waveguide and to two light detectors. The relative phase shift of the counter-propagating light signals in the primary waveguide is detected. The phase shift mea-surement is proportional to the physical inertial rotation of the sensor.
申请公布号 CA2052074(A1) 申请公布日期 1992.04.30
申请号 CA19912052074 申请日期 1991.09.23
申请人 HUGHES AIRCRAFT COMPANY 发明人 VALI, VICTOR;BROWNRIGG, PATRICK C.;CHANG, DAVID B.
分类号 G01C19/72;(IPC1-7):G01C19/64 主分类号 G01C19/72
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