Measuring and testing – Speed – velocity – or acceleration – Angular rate using gyroscopic or coriolis effect
Patent
1992-04-24
1993-06-15
Williams, Hezron E.
Measuring and testing
Speed, velocity, or acceleration
Angular rate using gyroscopic or coriolis effect
G01P 15125
Patent
active
052188671
ABSTRACT:
This invention relates to a single axis solid state attitude sensor in which, the spatial orientation of a resonant rode on a resonant body is maintained in alignment with the inertial angle K8 of the resonant body.
REFERENCES:
patent: 4079630 (1978-03-01), Friedland et al.
patent: 4157041 (1979-06-01), Loper, Jr. et al.
patent: 4793195 (1988-12-01), Koning
patent: 4951508 (1990-08-01), Loper, Jr. et al.
Langdon, R. M., "The Vibrating Cylinder Gyro," Marconi Review, 645, vol. 45 (1982) No. 227, Great Britain, pp. 231-249.
Day Charles
Hodgins Diana
Norris Timothy S.
Thomas Hugh D.
Varnham Malcolm P.
British Aerospace Public Limited Company
Finley Rose M.
Williams Hezron E.
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