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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|