Oscillating gyroscope

• US 5,915,275 A
• Filed: 06/27/1997
• Issued: 06/22/1999
• Est. Priority Date: 06/27/1996
• Status: Expired due to Fees

• Current Assignee: Milli Sensor Systems & Actuators, Inc.
• Original Assignee: Milli Sensor and Actuator Systems Incorporated
• Inventors: Cardarelli, Donato, Sapuppo, Michele
• Primary Examiner(s): Williams, Hezron
• Assistant Examiner(s): Kwok, Helen C.
• Application Number:
  US08/884,292
• Time in Patent Office: 725 Days
• Field of Search: 73/503.03, 73/504.02, 73/504.08, 73/504.09, 73/504.12, 73/504.18, 73/514.01, 73/514.02, 73/510, 74/5 R, 74/5.34
• US Class Current: 73/504.03
• CPC Class Codes: G01C 19/42 for indicating rate of turn; for integrating rate of turn

Abstract

An oscillatory gyroscope is described based on a three gimbal structure whose output is the rotary deflection of the middle gimbal. Closed loop operation is achieved by the oscillatory interaction between the outer and inner gimbals. The gyro is referred to as CLOG (Closed Loop Oscillating Gyro). Two variations on the manner of achieving the closed loop are also described. The gyro can be implemented in a three dimensional configuration or in three planar configurations which can be fabricated using modern photolithographic, batch process fabrication technology similar to MEMS.

Claims

1. A closed loop oscillating gyroscope for detecting motion about an input axis, comprising:

a fixed case;

a servo driven member mounted to said fixed case, for oscillation about a servo axis;

a torque summing member mounted to said servo driven member to allow rotational motion about an output axis corresponding to the gyroscope input axis, and transverse to said servo axis, wherein said rotational motion is induced as a result of gyroscope rotation about the gyroscope input axis;

a rotor driven member mounted to said torque summing member for oscillation about a reference axis transverse to both said output axis and said servo axis;

first oscillation means for oscillating said rotor driven member about said reference axis;

second oscillation means for oscillating said servo driven member about said servo axis;

means for sensing at least one aspect of the motion of at least one of said servo driven member and said torque summing member; and

means, responsive to said means for sensing, for determining the rotation of said fixed case about the input axis.

2. The closed loop oscillating gyroscope of claim 1 in which said means for sensing includes means for sensing rotational motion of said torque summing member about said output axis.

3. The closed loop oscillating gyroscope of claim 2 in which said second oscillation means is responsive to said means for sensing rotational motion of said torque summing member about said output axis.

4. The closed loop oscillating gyroscope of claim 3 wherein rotational motion of the gyroscope about the input axis induces oscillatory motion of said servo driven member, and in which said second oscillation means drives said servo driven member with a motion that is opposite in phase and equal in amplitude to said induced oscillatory motion, to cancel said induced oscillatory motion.

5. The closed loop oscillating gyroscope of claim 4 in which said means for sensing at least one aspect of the motion of at least one of said servo driven member and said torque summing member includes means for detecting the amplitude of said oscillatory motion of said servo driven member.

6. The closed loop oscillating gyroscope of claim 3 in which said first oscillation means and said second oscillation means oscillate said rotor driven member and said servo driven member, respectively, at the same oscillation frequency.

7. The closed loop oscillating gyroscope of claim 6 in which, when the gyroscope is not rotating about the gyroscope input axis, said oscillations of said rotor driven member and said servo driven member are 90°

out of phase.

8. The closed loop oscillating gyroscope of claim 7 in which said second oscillation means alters the phase of the servo driven member oscillation relative to the phase of the rotor driven member oscillation, to cancel rotational motion of said torque summing member induced as a result of gyroscope rotation about the gyroscope input axis.

9. The closed loop oscillating gyroscope of claim 8 in which said means for sensing at least one aspect of the motion of said at least one of said servo driven member and said torque summing member includes means for detecting the phase difference between the oscillations of said servo driven member and of said rotor driven member.

10. The closed loop oscillating gyroscope of claim 1 further including means for sensing at least one aspect of the oscillatory motion of said rotor driven member.

11. The closed loop oscillating gyroscope of claim 10 in which the oscillatory motion aspects sensed of both said rotor driven member and said servo driven member include oscillation phase.

12. The closed loop oscillating gyroscope of claim 10 in which said means for determining the rotation of said fixed case about the input axis is also responsive to said means for sensing at least one aspect of the oscillatory motion of said rotor driven member.

13. The closed loop oscillating gyroscope of claim 10 in which the oscillatory motion aspects sensed of both said rotor driven member and said servo driven member include oscillation amplitude.

14. The closed loop oscillating gyroscope of claim 1 in which said first oscillation means oscillates said rotor driven member at a fixed amplitude.

15. The closed loop oscillating gyroscope of claim 14 in which said first oscillation means oscillates said rotor driven member at a fixed phase, and said second oscillation means oscillates said servo driven member at a fixed phase 180°

different than said fixed phase of said rotor driven member oscillation.

16. The closed loop oscillating gyroscope of claim 14 in which said second oscillation means oscillates said servo driven member at resonance.

17. The closed loop oscillating gyroscope of claim 14 in which said means for sensing includes means for determining the angle of rotation of said torque summing member.

18. The closed loop oscillating gyroscope of claim 17 in which said means for determining the rotation of said fixed case about the input axis is responsive to said means for determining the angle of rotation of said torque summing member.

19. A closed-loop oscillating gyroscope for detecting motion about an input axis, comprising:

a fixed case;

a servo driven member mounted to said fixed case, for oscillation about a servo axis;

a torque summing member mounted to said servo driven member to allow rotational motion about an output axis corresponding to the gyroscope input axis, and transverse to said servo axis, wherein said rotational motion is induced as a result of gyroscope rotation about the gyroscope input axis;

a rotor driven member mounted to said torque summing member for oscillation about a reference axis transverse to both said output axis and said servo axis;

first oscillation means for sinusoidally oscillating said rotor driven member about said reference axis at a first frequency, first phase, and a first amplitude;

second oscillation means for sinusoidally oscillating said servo driven member about said servo axis at said first frequency and a second phase 180°

different than said first phase, and at said first amplitude;

first sensing means for sensing the amplitude and oscillation phase of the oscillatory motion of said servo driven member;

means, responsive to said first sensing means, for determining the rotation of said fixed case about the input axis;

second sensing means for sensing rotational motion of said torque summing member about said output axis; and

wherein said second oscillation means is responsive to said means for sensing rotational motion of said torque summing member about said output axis, and wherein rotational motion about the input axis induces oscillatory motion of said servo driven member in phase with the rotor driven member oscillation, and in which said second oscillation means in response drives said servo driven member with a motion that is opposite in phase and equal in amplitude to said induced oscillatory motion, to cancel said induced oscillatory motion.

20. A closed-loop oscillating gyroscope for detecting motion about an input axis, comprising:

a fixed case;

a servo driven member mounted to said fixed case, for oscillation about a servo axis;

a torque summing member mounted to said servo driven member to allow rotational motion about an output axis corresponding to the gyroscope input axis, and transverse to said servo axis, wherein said rotational motion is induced as a result of gyroscope rotation about the gyroscope input axis;

a rotor driven member mounted to said torque summing member for oscillation about a reference axis transverse to both said output axis and said servo axis;

first oscillation means for continuously, sinusoidally oscillating said rotor driven member about said reference axis at a first frequency;

second oscillation means for continuously, sinusoidally oscillating said servo driven member about said servo axis, the oscillation being at said first frequency, and 90°

out of phase with the oscillation of said rotor driven member, when the gyroscope is not rotating about the gyroscope input axis;

first sensing means for detecting the phase difference between the oscillations of said rotor driven member and said servo driven member;

means, responsive to said first sensing means, for determining the rotation of said fixed case about the input axis; and

second sensing means for sensing rotational motion of said torque summing member about said output axis;

wherein said second oscillation means is responsive to said means for sensing rotational motion of said torque summing member about said output axis, and wherein said second oscillation means alters the phase of the servo driven member oscillation relative to the phase of the rotor driven member oscillation, to cancel said rotational motion of said torque summing member induced as a result of gyroscope rotation about the gyroscope input axis.