Counterbalanced silicon tuned multiple accelerometer-gyro
AssigneeNorthrop Grumman Corporation
InventorsRobert E. Stewart, Stanley F. Wyse
Life of this patent
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AssigneeNorthrop Grumman Corporation
InventorsRobert E. Stewart, Stanley F. Wyse
Estimating the term…
A simplified and smaller accelerometer-gyro is provided by combining gyro and accelerometer functions in a single sensor unit which has a pair of counter oscillating accelerometers each having a pendulum or sense element and a vibrating element. The pendulum and vibrating element of each accelerometer are designed to be symmetrical so that the center of mass for each accelerometer are on a line which is parallel to the dither motion of the unit. The geometry of these two pendulums is configured so that the centers of percussion of each is at the same point. Electrodes on the top and bottom cover of the sensor unit combine the pickoff and forcing function with the pendulum tuning function, thereby simplifying electrical connection. A pair of mounting tabs are fastened to the frame by respective compliant beams. The accelerometer-gyro may be mounted in an enclosure that maintains a pressure below atmospheric around the accelerometer-gyro.
An accelerometer-gyro for sensing angular rate and acceleration having a structure formed from a substantially planar, monolithic material having first and second major surfaces, the accelerometer-gyro comprising:
Dependencies are inferred from the claim text.