Vibrating cylinder gyroscope and method

• US 4,793,195 A
• Filed: 10/20/1986
• Issued: 12/27/1988
• Est. Priority Date: 10/20/1986
• Status: Expired due to Fees

• Current Assignee: Northrop Corporation (Northrop Grumman Corporation)
• Original Assignee: Northrop Corporation (Northrop Grumman Corporation)
• Inventors: Koning, Menno G.
• Primary Examiner(s): Bonck, Rodney H.
• Application Number:
  US06/920,743
• Time in Patent Office: 799 Days
• Field of Search: 73/505, 73/517 AV, 73/688, 73/DIG. 1, 74/5.6 D, 74/5 R
• US Class Current: 74/5.60D
• CPC Class Codes: G01C 19/5691 of essentially three-dimensional vibrators, e.g. wine glass-type vibrators
• CPC Class Codes: Y10T 74/12 Gyroscopes
• CPC Class Codes: Y10T 74/1275 Electrical

Abstract

The gyroscope includes a symmetric and concentric, freely vibrating cylinder. Electromagnetic forcers are arranged to apply forces on the cylinder to excite the cylinder'"'"'s lowest order radially oscillating mode. The forcers also steer the resulting nodal pattern of the cylinder. The cylinder nodal pattern is sensed and a servo selectively excites the forcers to steer the nodal pattern to its original configuration in the presence of cylinder rotations. The forcer steering commands are related to the rotation rate of the gyro. The vibrating cylinder is free of any attachments or deposits and is machined accurately to eliminate the need for balancing, resulting in low temperature sensitivity.

Claims

1. Vibrating cylinder gyro comprising:

a cylinder;

electromagnetic forcers arranged to apply forces on the cylinder to excite its lowest order radially oscillating mode and to steer the resulting nodal pattern;

means for sensing the nodal pattern; and

servo means for controlling the forcers to steer the nodal pattern to its original configuration in the presence of cylinder rotations, the steering commands being related to rotation rate.

2. The gyro of claim 1 in which the cylinder is symmetric and concentric and free of any attachments or deposits.

3. The gyro of claim 1 further including a negative feedback loop to give minimum response time.

4. The gyro of claim 1 further including phase-locked drive circuits to maintain the drive frequency at the natural frequency to compensate for temperature variations.

5. The gyro of claim 1 in which the means for sensing the nodal pattern comprises capacitance or reluctance pickoffs.

6. Vibrating cylinder gyro comprising:

a ferromagnetic cylinder

electromagnetic forcers located inside the cylinder arranged to apply forces on the cylinder to excite its lowest order radially oscillating mode and to steer the resulting nodal pattern;

capacitance or reluctance pickoffs for sensing the nodal pattern; and

closed loop servo means for selectively exciting the forcers to steer the nodal pattern to an original configuration in the presence of cylinder rotations, the selective excitation being related to rotation rate.

7. A vibrating cylinder gyro for measuring angular rotation of a rotating platform comprising

a cylindrical shell mounted to the platform for movement therewith, said shell having an open end extending away from the platform, said end being free to resonate,

electrical transducer and drive current circuit means for exciting the shell to produce low order radial oscillations with nodes of vibration which move in response to rotational movement of the platform and shell,

pickoff means mounted to the platform and free of the shell for sensing movement of the nodes of vibration,

a servo loop means responsive to said pickoff means for regulating the electrical transducer current to move the nodes of vibration back to an original, unrotated position to thereby define a restore electrical current magnitude and phase, the values of which indicate the amount and direction or rotation of said platform and gyro.

8. In a method for measuring angular rotation of a rotating platform with a vibrating cylinder gyro including

a cylindrical shell mounted to the platform for movement therewith, said shell having an open end extending away from the platform, said end being free to resonate,

exciting the shell with an electrical transducer and drive current circuit means to produce low order radial oscillations with nodes of vibration which move in response to rotational movement of the platform and shell,

sensing movement of the nodes of vibration with pickoff means,

regulating the electrical transducer current with a servo loop means responsive to said pickoff means to move the nodes or vibration back to an original, unrotated position to thereby define a restore electrical current magnitude and phase, the values of which indicate the amount of rotation of said platform and gyro.