Micro-machined multi-sensor providing 1-axis of acceleration sensing and 2-axes of angular rate sensing

• US 6,837,107 B2
• Filed: 06/16/2003
• Issued: 01/04/2005
• Est. Priority Date: 04/28/2003
• Status: Active Grant

• Current Assignee: Analog Devices, Inc.
• Original Assignee: Analog Devices, Inc.
• Inventors: Geen, John A.
• Primary Examiner(s): CHAPMAN JR, JOHN E
• Application Number:
  US10/462,542
• Publication Number:
  US 20040211257A1
• Time in Patent Office: 568 Days
• Field of Search: 735/040.4, 735/041.2, 735/10
• US Class Current: 73/504.04
• CPC Class Codes: G01C 19/5712 the devices involving a micromechanical structure
• CPC Class Codes: G01P 15/125 by capacitive pick-up
• CPC Class Codes: G01P 15/14 by making use of gyroscopes gyroscopes per se G01C19/00

Abstract

A micro-machined multi-sensor that provides 1-axis of acceleration sensing and 2-axes of angular rate sensing. The multi-sensor includes a plurality of accelerometers, each including a mass anchored to and suspended over a substrate by a plurality of flexures. Each accelerometer further includes acceleration sense electrode structures disposed along lateral and longitudinal axes of the respective mass. The multi-sensor includes a fork member coupling the masses to allow relative antiphase movement, and to resist in phase movement, of the masses, and a drive electrode structure for rotationally vibrating the masses in antiphase. The multi-sensor provides electrically independent acceleration sense signals along the lateral and longitudinal axes of the respective masses, which are added and/or subtracted to obtain 1-axis of acceleration sensing and 2-axes of angular rate sensing.

Claims

1. A multi-sensor, comprising:

a substrate;

at least one first mass coupled to and suspended over the substrate, the first mass having associated longitudinal and lateral axes, and an associated rotation axis perpendicular to the longitudinal and lateral axes associated therewith;

at least one second mass coupled to and suspended over the substrate, the second mass having associated longitudinal and lateral axes, and an associated rotation axis perpendicular to the longitudinal and lateral axes associated therewith, the second mass being adjacent to the first mass,

at least one drive structure operatively coupled to the first and second masses, the drive structure being configured to vibrate the first and second masses in antiphase about the respective rotation axes;

first and second pairs of diametrically opposed acceleration sensing structures operatively coupled to the first mass, the first and second acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively, of the first mass; and

third and fourth pairs of diametrically opposed acceleration sensing structures operatively coupled to the second mass, the third and fourth acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively, of the second mass,

wherein the respective longitudinal and lateral axes associated with the first and second masses define a plane substantially parallel to a substrate plane,

wherein the respective longitudinal axes are parallel to a first rotation-sensing axis, and the respective lateral axes are parallel to a second rotation-sensing axis, the first and second rotation-sensing axes being substantially within the substrate plane,

wherein each acceleration sensing structure is configured to produce a respective sense signal, the respective sense signals including information pertaining to angular rate sensing relative to the first and second rotation-sensing axes, and further including information pertaining to acceleration sensing relative to an acceleration-sensing axis perpendicular to the substrate plane,

wherein each of the respective sense signals produced by the first and third pairs of acceleration sensing structures includes a linear component relative to the acceleration-sensing axis and a rotational component relative to the first rotation-sensing axis, and wherein each of the respective sense signals produced by the second and fourth pairs of acceleration sensing structures includes a linear component relative to the acceleration-sensing axis and a rotational component relative to the second rotation-sensing axis, and further including a signal processing unit configured to combine the respective linear sense signal components produced by the first, second, third, and fourth pairs of acceleration sensing structures to produce an output signal including information pertaining to acceleration sensing relative to the acceleration-sensing axis.

2. The multi-sensor of claim 1 wherein the signal processing unit is further configured to combine the respective rotational sense signal components produced by the first and third pairs of acceleration sensing structures to produce an output signal including information pertaining to angular rate sensing relative to the first rotation-sensing axis.

3. The multi-sensor of claim 1 wherein the signal processing unit is further configured to combine the respective rotational sense signal components produced by the second and fourth pairs of acceleration sensing structures to produce an output signal including information pertaining to angular rate sensing relative to the second rotation-sensing axis.

4. The multi-sensor of claim 1 further including a resilient member coupling the first mass and the second mass, the resilient member being configured to allow the antiphase vibrational movement, and to resist in phase vibrational movement, of the respective masses.

5. The multi-sensor of claim 1 including two first masses and two second masses suspended over the substrate, the four masses being arranged so that each mass is adjacent to two other masses, and wherein the drive structure is configured to vibrate the four masses in antiphase about the respective rotation axes so that each mass moves in an equal and opposite manner relative to an adjacent mass.

6. The multi-sensor of claim 1 wherein at least the first and second masses are micro-machined on the substrate, the first and second rotation-sensing axes being in the plane of the micro-machined substrate.

7. A multi-sensor, comprising:

a substrate;

at least one first mass coupled to and suspended over the substrate, the first mass having associated longitudinal and lateral axes, and an associated rotation axis perpendicular to the longitudinal and lateral axes associated therewith;

at least one second mass coupled to and suspended over the substrate, the second mass having associated longitudinal and lateral axes, and an associated rotation axis perpendicular to the longitudinal and lateral axes associated therewith, the second mass being adjacent to the first mass,

at least one drive structure operatively coupled to the first and second masses, the drive structure being configured to vibrate the first and second masses in antiphase about the respective rotation axes;

first and second pairs of diametrically opposed acceleration sensing structures operatively coupled to the first mass, the first and second acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively, of the first mass; and

third and fourth pairs of diametrically opposed acceleration sensing structures operatively coupled to the second mass, the third and fourth acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively, of the second mass,

wherein the respective longitudinal and lateral axes associated with the first and second masses define a plane substantially parallel to a substrate plane;

wherein the respective longitudinal axes are parallel to a first rotation-sensing axis, and the respective lateral axes are parallel to a second rotation-sensing axis, the first and second rotation-sensing axes being substantially within the substrate plane,

wherein each acceleration sensing structure is configured to produce a respective sense signal, the respective sense signals including information pertaining to angular rate sensing relative to the first and second rotation-sensing axes, and further including information pertaining to acceleration sensing relative to an acceleration-sensing axis perpendicular to the substrate plane, and

further including a first amplifier configured to receive a pair of first sense signals from the first pair of acceleration sensing structures, and a third amplifier configured to receive a pair of third sense signals from the third pair of acceleration sensing structures, the first and third amplifiers being further configured to produce first and third output signals comprising the difference of the pair of first sense signals, and the difference of the pair of third sense signals, respectively, the first and third output signals including information pertaining to angular rate sensing relative to the first rotation-sensing axis.

8. A multi-sensor, comprising:

a substrate;

at least one first mass coupled to and suspended over the substrate, the first mass having associated longitudinal and lateral axes, and an associated rotation axis perpendicular to the longitudinal and lateral axes associated therewith;

at least one second mass coupled to and suspended over the substrate, the second mass having associated longitudinal and lateral axes, and an associated rotation axis perpendicular to the longitudinal and lateral axes associated therewith, the second mass being adjacent to the first mass,

at least one drive structure operatively coupled to the first and second masses, the drive structure being configured to vibrate the first and second masses in antiphase about the respective rotation axes;

first and second pairs of diametrically opposed acceleration sensing structures operatively coupled to the first mass, the first and second acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively, of the first mass; and

third and fourth pairs of diametrically opposed acceleration sensing structure operatively coupled to the second mass, the third and fourth acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively, of the second mass,

wherein the respective longitudinal and lateral axes associated with the first and second masses define a plane substantially parallel to a substrate plane;

wherein the respective longitudinal axes are parallel to a first rotation-sensing axis, and the respective lateral axes are parallel to a second rotation sensing axis, the first and second rotation-sensing axes being substantially within the substrate plane,

wherein each acceleration sensing structure is configured to produce a respective sense signal, the respective sense signals including information pertaining to angular rate sensing relative to the first and second rotation-sensing axes, and further including information pertaining to acceleration sensing relative to an acceleration-sensing axis perpendicular to the substrate plane, and

further including a second amplifier configured to receive a pair of second sense signals from the second pair of acceleration sensing structures, and a fourth amplifier configured to receive a pair of fourth sense signals from the fourth pair of acceleration sensing structures, the second and fourth amplifiers being further configured to produce second and fourth output signals comprising the difference of the pair of second sense signals, and the difference of the pair of fourth sense signals, respectively, the second and fourth output signals including information pertaining to angular rate sensing relative to the second rotation-sensing axis.

9. A multi-sensor, comprising:

a substrate;

at least one first mass coupled, to and suspended over the substrate, the first mass having associated longitudinal and lateral axes, and an associated rotation axis perpendicular to the longitudinal and lateral axes associated therewith;

at least one second mass coupled to and suspended over the substrate, the second mass having associated longitudinal and lateral axes, and an associated rotation axis perpendicular to the longitudinal and lateral axes associated therewith, the second mass being adjacent to the first mass,

at least one drive structure operatively coupled to the first and second masses, the drive structure being configured to vibrate the first and second masses in antiphase about the respective rotation axes;

first and second pairs of diametrically opposed acceleration sensing structures operatively coupled to the first mass, the first and second acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively, of the first mass; and

third and fourth pairs of diametrically opposed acceleration sensing structures operatively coupled to the second mass, the third and fourth acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively, of the second mass,

wherein the respective longitudinal and lateral axes associated with the first and second masses define a plane substantially parallel to a substrate plane;

wherein the respective longitudinal axes are parallel to a first rotation-sensing axis, and the respective lateral axes are parallel to a second rotation-sensing axis, the first and second rotation-sensing axes being substantially within the substrate plane,

wherein each acceleration sensing structure is configured to produce a respective sense signal, the respective sense signals including information pertaining to angular rate sensing relative to the first and second rotation-sensing axes, and further including information pertaining to acceleration sensing relative to an acceleration-sensing axis perpendicular to the substrate plane, and

further including a first amplifier configured to receive a pair of first sense signals from the first pair of acceleration sensing structures, a second amplifier configured to receive a pair of second sense signals from the second pair of acceleration sensing structures, a third amplifier configured to receive a pair of third sense signals from the third pair of acceleration sensing structures, and a fourth amplifier configured to receive a pair of fourth sense signals from the fourth pair of acceleration sensing structures, the first, second, third, and fourth amplifiers being further configured to produce first, second, third, and fourth output signals comprising the sum of the pair of first sense signals, the sum of the pair of second sense signals, the sum of the pair of third sense signals, and the sum of the pair of fourth sense signals, respectively, the first, second, third, and fourth output signals including information pertaining to acceleration sensing relative to the acceleration-sensing axis.

10. A method of operating a multi-sensor, comprising the steps of:

vibrating in antiphase at least one first mass and at least one second mass about respective rotation axes by a drive structure, the first and second masses being adjacent to each other and being coupled to and suspended over a substrate, each mass having associated longitudinal and lateral axes perpendicular to the respective rotation axis,

wherein the respective longitudinal and lateral axes associated with the first and second masses define a plane substantially parallel to a substrate plane, the respective longitudinal axes being parallel to a first rotation-sensing axis, and the respective lateral axes being parallel to a second rotation-sensing axis, the first and second rotation-sensing axes being substantially within the substrate plane;

producing respective sense signals by first and second pairs of diametrically opposed acceleration sensing structures operatively coupled to the first mass, the first and second acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively, of the first mass; and

producing respective sense signals by third and fourth pairs of diametrically opposed acceleration sensing structures operatively coupled to the second mass, the third and fourth acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively, of the second mass,

wherein the respective sense signals produced in the first and second producing steps include information pertaining to angular rate sensing relative to the first and second rotation-sensing axes, and further include information pertaining to acceleration sensing relative to an acceleration-sensing axis perpendicular to the substrate plane,

wherein each of the respective sense signals produced by the first and third pairs of acceleration sensing structures in the first and second producing steps includes a linear component relative to the acceleration-sensing axis and a rotational component relative to the first rotation-sensing axis, and wherein each of the respective sense signals produced by the second and fourth pairs of acceleration sensing structures in the first and second producing steps includes a linear component relative to the acceleration-sensing axis and a rotational component relative to the second rotation-sensing axis, and

further including the step of combining the respective linear sense signal components produced by the first, second, third, and fourth pairs of acceleration sensing structures by a signal processing unit to produce an output signal including information pertaining to acceleration sensing relative to the acceleration-sensing axis.

11. The method of claim 10 further including the step of combining the respective rotational sense signal components produced by the first and third pairs of acceleration sensing structures by the signal processing unit to produce an output signal including information pertaining to angular rate sensing relative to the first rotation-sensing axis.

12. The method of claim 10 further including the step of combining the respective rotational sense signal components produced by the second and fourth pairs of acceleration sensing structures by the signal processing unit to produce an output signal including information pertaining to angular rate sensing relative to the second rotation-sensing axis.

13. The method of claim 10 wherein the vibrating step includes vibrating two first masses and two second masses in antiphase about the respective rotation axes by a drive structure, the four masses being suspended over the substrate, the four masses being arranged so that each mass is adjacent to two other masses, the four masses being vibrated by the drive structure so that each mass moves in an equal and opposite manner relative to an adjacent mass.

14. A method of operating a multi-sensor, comprising the steps of:

vibrating in antiphase at least one first mass and at least one second mass about respective rotation axes by a drive structure, the first and second masses being adjacent to each other and being coupled to and suspended over a substrate, each mass having associated longitudinal and lateral axes perpendicular to the respective rotation axis,

wherein the respective longitudinal and lateral axes associated with the first and second masses define a plane substantially parallel to a substrate plane, the respective longitudinal axes being parallel to a first rotation-sensing axis, and the respective lateral axes being parallel to a second rotation-sensing axis, the first and second rotation-sensing axes being substantially within the substrate plane;

producing respective sense signals by first and second pairs of diametrically opposed acceleration sensing structures operatively coupled to the first mass, the first and second acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively, of the first mass; and

producing respective sense signals by third and fourth pairs of diametrically opposed acceleration sensing structures operatively coupled to the second mass, the third and fourth acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively, of the second mass,

wherein the respective sense signals produced in the first and second producing steps include information pertaining to angular rate sensing relative to the first and second rotation-sensing axes, and further include information pertaining to acceleration sensing relative to an acceleration-sensing axis perpendicular to the substrate plane, and

further including the steps of receiving a pair of first sense signals from the first pair of acceleration sensing structures by a first amplifier, receiving a pair of third sense signals from the third pair of acceleration sensing structures by a third amplifier, and producing first and third output signals comprising the difference of the pair of first sense signals, and the difference of the pair of third sense signals, respectively, by the first and third amplifiers, the first and third output signals including information pertaining to angular rate sensing relative to the first rotation-sensing axis.

15. A method of operating a multi-sensor, comprising the steps of:

vibrating in antiphase at least one first mass and at least one second mass about respective rotation axes by a drive structures, the first and second masses being adjacent to each other and being coupled to and suspended over a substrate, each mass having associated longitudinal and lateral axes perpendicular to the respective rotation axis,

wherein the respective longitudinal and lateral axes associated with the first and second masses define a plane substantially parallel to a substrate plane, the respective longitudinal axes being parallel to a first rotation-sensing axis, and the respective lateral axes being parallel to a second rotation-sensing axis, the first and second rotation-sensing axes being substantially within the substrate plane;

producing respective sense signals by first and second pairs of diametrically opposed acceleration sensing structures operatively coupled to the first mass, the first and second acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively of the first mass; and

producing respective sense signals by third and fourth pairs of diametrically opposed acceleration sensing structures operatively coupled to the second mass, the third and fourth acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively, of the second mass,

wherein the respective sense signals produced in the first and second producing steps include information pertaining to angular rate sensing relative to the first and second rotation-sensing axes, and further include information pertaining to acceleration sensing relative to an acceleration-sensing axis perpendicular to the substrate plane, and

further including the steps of receiving a pair of second sense signals from the second pair of acceleration sensing structures by a second amplifier, receiving a pair of fourth sense signals from the fourth pair of acceleration sensing structures by a fourth amplifier, and producing second and fourth output signals comprising the difference of the pair of second sense signals, and the difference of the pair of fourth sense signals, respectively, by the second and fourth amplifiers, the second and fourth output signals including information pertaining to angular rate sensing relative to the second rotation-sensing axis.

16. A method of operating a multi-sensor, comprising the steps of:

vibrating in antiphase at least one first mass and at least one second mass about respective rotation axes by a drive structure, the first and second masses being adjacent to each other and being coupled to and suspended over a substrate, each mass having associated longitudinal and lateral axes perpendicular to the respective rotation axis,

wherein the respective longitudinal and lateral axes associated with the first and second masses define a plane substantially parallel to a substrate plane, the respective longitudinal axes being parallel to a first rotation-sensing axis, and the respective lateral axes being parallel to a second rotation-sensing axis, the first and second rotation-sensing axes being substantially within the substrate plane;

producing respective sense signals by first and second pairs of diametrically opposed acceleration sensing structures operatively coupled to the first mass, the first and second acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively, of the first mass; and

producing respective sense signals by third and fourth pairs of diametrically opposed acceleration sensing structures operatively coupled to the second mass, the third and fourth acceleration sensing structure pairs being disposed along the longitudinal and lateral axes, respectively, of the second mass,

wherein the respective sense signals produced in the first and second producing steps include information pertaining to angular rate sensing relative to the first and second rotation-sensing axes, and further include information pertaining to acceleration sensing relative to an acceleration-sensing axis perpendicular to the substrate plane, and

further including the steps of receiving a pair of first sense signals from the first pair of acceleration sensing structures by a first amplifier, receiving a pair of second sense signals from the second pair of acceleration sensing structures by a second amplifier, receiving a pair of third sense signals from the third pair of acceleration sensing structures by a third amplifier, receiving a pair of fourth sense signals from the fourth pair of acceleration sensing structures by a fourth amplifier, and producing first, second, third, and fourth output signals comprising the sum of the pair of first sense signals, the sum of the pair of second sense signals, the sum of the pair of third sense signals, and the sum of the pair of fourth sense signals, respectively, by the first, second, third, and fourth amplifiers, the first, second, third, and fourth output signals including information pertaining to acceleration sensing relative to the acceleration-sensing axis.