Self-calibrating accelerometer
View Patent ↗The method and apparatus in one embodiment may have: a sensing element for an accelerometer having a bias, the sensing element having a rectangular plate supported by flexures which allow rotation about a transverse center line thereof; a center of mass (CG) of the sensing element having two stable positions, one on each side of an axis of rotation defined by a centerline of suspension; a secondary mass within a proofmass translates in-plane to move the center of mass to thereby effect a self-calibration mechanization that continuously measures and nulls the accelerometer's bias under dynamic operating conditions.
1. An apparatus, comprising:
a sensing element for an accelerometer having a bias, the sensing element having a plate supported by flexures which allow rotation about a transverse center line thereof;
a center of mass (CG) of the sensing element having two stable positions, one on each side of an axis of rotation defined by a centerline of suspension;
a secondary mass within a proofmass translates in-plane to move the center of mass to thereby effect a self-calibration mechanization that continuously measures and nulls the accelerometer's bias under dynamic operating conditions.
2. The apparatus according to claim 1 , wherein the secondary mass within the proofmass translates in-plane to move the center of mass right and left.
3. The apparatus according to claim 1 , wherein the center of mass is relocated from one side of the centerline of suspension to the other side to thereby reverse a polarity of an input axis to enable self-calibration of accelerometer bias.
4. The apparatus according to claim 1 , wherein under acceleration the sensing element is rotatable clockwise about a centerline of support (CS) with the center of mass in a first center of mass (CG1) position and counter clockwise with the center of mass in a second center of mass (CG2) position.
5. The apparatus according to claim 4 , wherein to change polarity of the accelerometer, the centers of mass (CG1 and CG2) are vertically moveable between two bistable positions above and below a centerline of suspension (CS) of the sensing element.
6. The apparatus according to claim 5 , wherein the secondary mass is translated up and down out-of-plane.
7. A method, comprising:
continuously self-calibrating accelerometer bias under both static and dynamic conditions to thereby remove accelerometer bias as an error source;
successively and simultaneously measuring acceleration by two accelerometers with sequentially alternating polarities; and
processing the measured acceleration from the outputs of the accelerometers in a digital signal processor using a real time bias estimator algorithm to thereby effect the bias self-calibration.
8. The method according to claim 7 , wherein the alternating polarity reversal is accomplished by alternating a location of a center of mass of a sensing element to opposite sides of a centerline of support of the sensing element.
9. The method according to claim 7 , wherein the method further comprises translating a secondary mass within a proofmass in-plane to move a center of mass right and left.
10. The method according to claim 9 , wherein the method further comprises relocating the center of mass from one side of the centerline of suspension to the other side to thereby reverse a polarity of an input axis to enable self-calibration of accelerometer bias.
11. The method according to claim 9 , wherein the method further comprises, under acceleration, rotating the sensing element clockwise about a centerline of support (CS) with the center of mass in a first center of mass (CG1) position and counter clockwise with the center of mass in a second center of mass (CG2) position.
12. The method according to claim 11 , wherein to change polarity of the accelerometer, the centers of mass (CG1 and CG2) are vertically moveable between two bistable positions above and below a centerline of suspension (CS) of the sensing element.
13. The method according to claim 12 , wherein the secondary mass is translated up and down out-of-plane.
14. An apparatus, comprising:
a sensing element in which a secondary mass is suspended within a proofmass of the sensing element for an accelerometer; and
a pair of buckled beam flexures that suspend the secondary mass within the proofmass, the suspension allowing the secondary mass to be in one of two bi-stable positions;
thereby effecting a self-calibration mechanization that continuously measures and nulls the accelerometer's bias under dynamic operating conditions.
15. The apparatus according to claim 14 , wherein the apparatus further comprises thermal actuators that reduce compressive force in the buckled beams allowing the secondary mass to move from one position of the two bi-stable positions to the other position of the bi-stable positions.
16. The apparatus according to claim 14 , wherein a secondary mass is translatable within the proofmass in-plane to move a center of mass right and left.
17. The apparatus according to claim 14 , wherein the apparatus further comprises relocating a center of mass from one side of the centerline of suspension of the secondary mass to the other side to thereby reverse a polarity of an input axis to enable self-calibration of accelerometer bias.
18. The apparatus according to claim 14 , wherein the apparatus further comprises, under acceleration, rotating the sensing element clockwise about a centerline of support (CS) with the center of mass in a first center of mass (CG1) position and counter clockwise with the center of mass in a second center of mass (CG2) position.
19. The apparatus according to claim 18 , wherein to change polarity of the accelerometer, the centers of mass (CG1 and CG2) are vertically moveable between two bistable positions above and below a centerline of suspension (CS) of the sensing element.
20. The apparatus according to claim 19 , wherein the secondary mass is translated up and down out-of-plane.