Approach for control redistribution of coriolis vibratory gyroscope (CVG) for performance improvement

Patent metadata

Field	Value
Publication number	US-9709399-B2
Application number	US-201514594893-A
Country	US
Kind code	B2
Filing date	Jan 12, 2015
Priority date	Jan 12, 2015
Publication date	Jul 18, 2017
Grant date	Jul 18, 2017

Abstract

Provided herein is a Coriolis vibratory gyroscope (“CVG”). The CVG includes a first plurality of actuators electrically coupled to the vibratory member and arranged about a drive axis of the CVG and operable to obtain a control signal from the controller and provide a voltage sufficient to cause and maintain the vibratory member to vibrate in a first mode of oscillation; a second plurality of actuators electrically coupled to the vibratory member and arranged about a sense axis of the CVG and operable to detect a voltage based on a second mode of oscillation of the vibratory member caused by a rotation of the CVG about an axis of rotation and to provide a counter-balancing signal sufficient to null the voltage based on the second mode of oscillation, wherein the controller is operable to determine a rate of the rotation of the CVG based, in part, on the counter-balancing signal.

First claim

What is claimed is:

1. A Coriolis vibratory gyroscope (“CVG”) comprising:
a vibratory member;
a controller;
a first actuator and a second actuator electrically coupled to the vibratory member, wherein the first actuator and the second actuator are offset from a drive axis of the CVG, arranged on opposite sides of the drive axis, and operable to obtain a control signal from the controller and provide a first voltage to the controller sufficient to cause and maintain the vibratory member to vibrate in a first mode of oscillation; and
a third actuator and a fourth actuator electrically coupled to the vibratory member, wherein the third actuator and the fourth actuator are offset from a sense axis of the CVG, arranged on opposite sides of the sense axis, and operable to detect a second voltage based on a second mode of oscillation of the vibratory member caused by a rotation of the CVG about an axis of rotation and provide a counter-balancing signal to the controller sufficient to nullify the second voltage based on the second mode of oscillation, wherein the sense axis is orthogonal to the drive axis in a modal reference frame,
wherein the controller is operable to determine a rate of the rotation of the CVG based, in part, on the counter-balancing signal,
wherein the controller is operable to modify the control signal to the first actuator or the second actuator by a corresponding first weighting factor or second weighting factor to compensate for misalignments in placement of the first actuator or the second actuator relative to the vibratory member.

2. The CVG of claim 1 , wherein the vibratory member is symmetric relative to the sense axis and the drive axis.

3. The CVG of claim 1 , wherein the controller is operable to modify the counter-balancing signal to the third actuator or the fourth actuator by a corresponding first or second weighting factor to compensate for misalignments in placement of the third actuator or the fourth actuator relative to the vibratory member.

4. The CVG of claim 3 , wherein the controller is operable to preset the first weighting factor or the second weighting factor and the third weighting factor or the fourth weighting factor by a same amount.

5. The CVG of claim 3 , wherein the controller is operable to adjust the third weighting factor or the fourth weighting factor and a physical misalignment and damping asymmetry such that a bias of the CVG is minimized or eliminated.

6. The CVG of claim 1 , wherein the controller is operable to adjust the first weighting factor or the second weighting factor based on a detected misalignment between the control signal and a voltage measured at a pickoff associated with the drive axis.

7. The CVG of claim 1 , wherein the controller is operable to adjust the third weighting factor or the fourth weighting factor and a physical misalignment and damping asymmetry such that a bias of the CVG is minimized or eliminated.

8. A method of compensating for bias in a Coriolis vibratory gyroscope (“CVG”), the CVG comprising a vibratory member, a controller, a first actuator and a second actuator coupled to the vibratory member, wherein the first actuator and the second actuator are offset from and on opposite sides of a drive axis of the CVG, and a third actuator and a fourth actuator coupled to the vibratory member, wherein the third actuator and the fourth actuator are offset from and on opposite sides of a sense axis of the CVG, wherein the drive axis and the sense axis are orthogonal to each other in a modal reference frame, the method comprising:
obtaining, from the controller, a first control signal from the controller to provide a first voltage sufficient to cause and maintain the vibratory member to vibrate in a first mode of oscillation;
detecting, by the controller, a second voltage based on a second mode of oscillation of the vibratory member caused by a rotation of the CVG about an axis of rotation;
providing, by the controller, a counter-balancing signal sufficient to nullify the second voltage based on the second mode of oscillation;
determining, by the controller, a rate of the rotation of the CVG based, in part, on the counter-balancing signal; and
modifying, by the controller, the control signal to the first actuator or the second actuator by a corresponding first weighting factor or a second weighting factor to compensate for misalignments in placement of the first actuator or the second actuator relative to the vibratory member.

9. The method of claim 8 , wherein the vibratory member is symmetric relative to the sense and the drive axis.

10. The method of claim 8 , further comprising modifying, by the controller, the counter-balancing signal to the third actuator or the fourth actuator by a corresponding third weighting factor or a fourth weighting factor to compensate for misalignments in placement of the third actuator or the fourth actuator relative to the vibratory member.

11. The method of claim 10 , further comprising setting, by the controller, the first weighting factor or the second weighting factor and the third weighting factor or the fourth weighting factor to a same amount.

12. The method of claim 10 , further comprising adjusting, by the controller, the third weighting factor or the fourth weighting factor and a physical misalignment and damping asymmetry such that a bias of the CVG is minimized or eliminated.

13. The method of claim 8 , further comprising adjusting, by the controller, the first weighting factor or the second weighting factor based on a detected misalignment between the control signal and a voltage measured at a pickoff associated with the drive axis.

14. The method of claim 8 , further comprising adjusting, by the controller, the first weighting factor or the second weighting factor and a physical misalignment and damping asymmetry such that a bias of the CVG is minimized or eliminated.

Assignees

• Boeing Co

Inventors

• Liu John Y

Classifications

• G01C19/5719

  using planar vibrating masses driven in a translation vibration along an axis · CPC title

• G01C19/5705

  using masses driven in reciprocating rotary motion about an axis · CPC title

• G01C19/56 Primary

  Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces · CPC title

• G01C19/5663 Primary

  Manufacturing; Trimming; Mounting; Housings · CPC title

• G01C19/5776 Primary

  Signal processing not specific to any of the devices covered by groups G01C19/5607 - G01C19/5719 · CPC title