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US 4,270,387 AGranted
Drift compensated gyroscope
AssigneeThe Singer Company
InventorJay Hoffman
Life of this patent
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Abstract
A gyroscope which has a spinning fluid filled annulus as an inertial angle rate sensor is compensated for inertial drift by resolving an output signal from the sensor into acceleration proportional components related to the gimbal axes and the component related to the inner axis is applied to the outer axis, and the component related to the outer axis is applied to the inner axis to cancel out the effects of drift.
Claims4
A drift compensated gyroscope including:
- an inertial angle rate sensor comprising a fluid filled annulus mounted for rotation about an axis perpendicular to the axis of rotation of the sensor on the inner of a double set of gimbals and having an output signal proportional to the angular rate of the sensor, means for rotating the sensor about the axis of rotation of the sensor;
- means for resolving the output signal into components related to the gimbal axes and applying substantially equal and opposite rates proportional to the components to the gimbal axes to cancel out the effects of drift, and
- means for measuring the gimbal inertial angles.
The method of correcting a doubly gimballed gyroscope for drift comprising:
- (a) mounting a fluid filled annulus for rotation about an axis perpendicular to the axis of rotation to be sensed on the inner of a double set of gimbals;
- (b) spinning said fluid containing annulus;
- (c) generating a signal porportional to the drift induced angular rate experienced by the gyroscope with said fluid containing annulus;
- (d) resolving the signal into components related to the gimbal axes;
- and
- (e) applying torque proportional to each component to the opposite gimbal axis, by torquers, so as to produce a rate of the gyroscope which is equal and opposite to that induced by the drift.
3 more elements
Dependencies are inferred from the claim text.