Accelerometer compensation in an inertial navigation system

• US 6,634,207 B1
• Filed: 10/10/2000
• Issued: 10/21/2003
• Est. Priority Date: 10/10/2000
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Litton Systems Incorporated
• Inventors: Tazartes, Daniel A., Lottman, Brian T.
• Primary Examiner(s): NOLAND, THOMAS
• Application Number:
  US09/686,165
• Time in Patent Office: 1,106 Days
• Field of Search: 73/17.8, 73/13.8, 702/93, 702/92, 702/94, 702/96, 702/141, 702/147, 702/151, 702/153, 702/196
• US Class Current: 73/1.78
• CPC Class Codes: G01C 21/183 Compensation of inertial measurements, e.g. for temperature effects
• CPC Class Codes: G01C 25/00 Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass testing, calibrating or compensating compasses G01C17/38

Abstract

The invention is a method and apparatus for improving the accuracy of an inertial navigation system. The method comprises (1) obtaining a measure of the angular velocity of a body frame of reference having a first axis, a second axis, and a third axis, (2) obtaining a measure of the acceleration of a first reference point in the direction of the first axis, a second reference point in the direction of the second axis, and a third reference point in the direction of the third axis, the first, second, and third reference points being fixed in the body frame, and (3) determining compensated acceleration values. A compensated acceleration value is the difference of the measure of acceleration of a reference point and a compensation quantity. A compensation quantity is an estimate of the portion of the acceleration of the reference point resulting from the rotation of the body frame. The method further comprises establishing the optimum navigation center based on a criterion of goodness. The criterion of goodness is minimal weighted acceleration error where acceleration error is a function of the direction of the angular velocity vector and weighted acceleration error is obtained by multiplying the acceleration error by a weighting function and integrating the result over all directions of the angular velocity vector.

Claims

1. A method for improving the accuracy of an inertial navigation system, the method comprising the steps:

obtaining a measure of the angular velocity of a body frame of reference having a first axis, a second axis, and a third axis;

obtaining a measure of the acceleration of (1) a first reference point in the direction of the first axis, (2) a second reference point in the direction of the second axis, and (3) a third reference point in the direction of the third axis, the first, second, and third reference points being fixed in the body frame;

determining compensated acceleration values, a compensated acceleration value being the difference of the measure of acceleration of a reference point and a compensation quantity, the compensation quantity being an estimate of the portion of the acceleration of the reference point resulting from the rotation of the body frame.

2. The method of claim 1 wherein the compensation quantity comprises a compensation term proportional to the vector cross product of a first vector and a second vector, the first vector being the angular velocity of the body frame, the second vector being the cross product of the angular velocity of the body frame and the vector connecting the navigation center to a reference point, an estimate of the angular velocity of the body frame being obtained by multiplying each of a plurality of measures of the angular velocity obtained at regular intervals in the past by a weight and summing the weighted measures of the angular velocity obtained during a specified time period in the past.

3. The method of claim 2 wherein the weights are all equal.

4. The method of claim 1 wherein the compensation quantity comprises a compensation term proportional to the cross product of the angular acceleration of the body frame and the vector connecting the navigation center to a reference point, an estimate of the angular acceleration of the body frame being obtained by multiplying each of a plurality of measures of the angular velocity obtained at regular intervals in the past by a weight and summing the weighted measures of the angular velocity obtained during a specified time period in the past.

5. The method of claim 4 wherein an estimate of the angular acceleration of the body frame is obtained by differencing first and second estimates of the angular velocity of the body frame, a first estimate of the angular velocity of the body being obtained by multiplying a first sequence of measures of the angular velocity obtained at regular intervals in the past by a first sequence of weights and summing the resulting first sequence of weighted measures of the angular velocity obtained during a specified time period in the past, a second estimate of the angular velocity of the body being obtained by multiplying a second sequence of measures of the angular velocity obtained at regular intervals in the past by a second sequence of weights and summing the resulting second sequence of weighted measures of the angular velocity obtained during a specified time period in the past.

6. The method of claim 5 wherein the first and second sequences of weights are the same.

7. The method of claim 6 wherein the weights in the first and second sequences of weights are all equal.

8. The method of claim 1 further comprising the step:

establishing the optimum navigation center based on a criterion of goodness.

9. The method of claim 8 wherein the criterion of goodness is minimal weighted acceleration error, acceleration error being a function of the direction of the angular velocity vector, weighted acceleration error being obtained by multiplying the acceleration error by a weighting function and integrating the result over all directions of the angular velocity vector.

10. The method of claim 9 wherein the weighting function has the same value for all directions of the angular velocity vector.

11. Apparatus for improving the accuracy of an inertial navigation system, the apparatus comprising:

a means for obtaining from an external source a measure of the angular velocity of a body frame of reference having a first axis, a second axis, and a third axis;

a means for obtaining from an external source a measure of the acceleration of (1) a first reference point in the direction of the first axis, (2) a second reference point in the direction of the second axis, and (3) a third reference point in the direction of the third axis, the first, second, and third reference points being fixed in the body frame;

a processor for determining compensated acceleration values, a compensated acceleration value being the difference of the measure of acceleration of a reference point and a compensation quantity, the compensation quantity being an estimate of the portion of the acceleration of the reference point resulting from the rotation of the body frame.

12. The apparatus of claim 11 wherein the compensation quantity comprises a compensation term proportional to the vector cross product of a first vector and a second vector, the first vector being the angular velocity of the body frame, the second vector being the cross product of the angular velocity of the body frame and the vector connecting the navigation center to a reference point, an estimate of the angular velocity of the body frame being obtained by multiplying each of a plurality of measures of the angular velocity obtained at regular intervals in the past by a weight and summing the weighted measures of the angular velocity obtained during a specified time period in the past.

13. The apparatus of claim 11 wherein the weights are all equal.

14. The apparatus of claim 11 wherein the compensation quantity comprises a compensation term proportional to the cross product of the angular acceleration of the body frame and the vector connecting the navigation center to a reference point, an estimate of the angular acceleration of the body frame being obtained by multiplying each of a plurality of measures of the angular velocity obtained at regular intervals in the past by a weight and summing the weighted measures of the angular velocity obtained during a specified time period in the past.

15. The apparatus of claim 11 wherein an estimate of the angular acceleration of the body frame is obtained by differencing first and second estimates of the angular velocity of the body frame, a first estimate of the angular velocity of the body being obtained by multiplying a first sequence of measures of the angular velocity obtained at regular intervals in the past by a first sequence of weights and summing the resulting first sequence of weighted measures of the angular velocity obtained during a specified time period in the past, a second estimate of the angular velocity of the body being obtained by multiplying a second sequence of measures of the angular velocity obtained at regular intervals in the past by a second sequence of weights and summing the resulting second sequence of weighted measures of the angular velocity obtained during a specified time period in the past.

16. The apparatus of claim 15 wherein the first and second sequences of weights are the same.

17. The apparatus of claim 16 wherein the weights in the first and second sequences of weights are all equal.

18. The apparatus of claim 11 wherein the optimum navigation center is based on a criterion of goodness.

19. The apparatus of claim 18 wherein the criterion of goodness is minimal weighted acceleration error, acceleration error being a function of the direction of the angular velocity vector, weighted acceleration error being obtained by multiplying the acceleration error by a weighting function and integrating the result over all directions of the angular velocity vector.

20. The apparatus of claim 19 wherein the weighting function has the same value for all directions of the angular velocity vector.