Method and apparatus for automatic calibration of magnetic compass

• US 4,611,293 A
• Filed: 11/28/1983
• Issued: 09/09/1986
• Est. Priority Date: 11/28/1983
• Status: Expired due to Term

• Current Assignee: Mesc Electronic Systems, Inc.
• Original Assignee: Magnavox Government and Industrial Electronics Company
• Inventors: Hatch, Ronald R., Keegan, Richard G.
• Primary Examiner(s): Gruber, Felix D.
• Application Number:
  US06/555,885
• Time in Patent Office: 1,016 Days
• Field of Search: 364/556, 364/559, 364/571, 324/244, 324/245, 33/355 R, 33/356, 33/357
• US Class Current: 702/92
• CPC Class Codes: G01C 17/38 Testing, calibrating, or compensating of compasses

Abstract

A three winding induction compass mounted in a host vehicle has each winding output coupled to an analog to digital converter. Each winding output is weighted and accumulated by a push down stack circuit to obtain a time filtered output and the maximum and minimum values of each filtered output are determined and stored as the vehicle is turned in a 360° circle. The distortions due to the permanent and induced magnetism of the host vehicle and due to winding imbalance between the three windings and misorientation of the three windings are obtained from the maximum and minimum values to obtain calibration parameters. The calibration parameters for the windings are applied to the outputs of the three windings to obtain an equivalent two winding output which is normalized for determining the corrected compass heading.

Claims

1. Apparatus for calibrating the distortions in the readings of a magnetic compass having a plurality of windings in a two dimensional plane and mounted in a vehicle comprising:

first means coupled to the compass windings for obtaining the outputs from each of the windings as a function of time by weighting and combining the outputs from each of the windings at a first time and for a predetermined number of the next previous times to said first time to obtain a time filtered output for each of the windings;

second means coupled to said first means for receiving the time filtered outputs and for obtaining maximum and minimum filtered outputs for each of the windings as the vehicle is turned through a circle of 360°

;

third means coupled to said second means for computing biases from the maximum and minimum filtered outputs equal to the average of the maximum and minimum filtered outputs from each winding;

fourth means coupled to said third means for applying said biases to said maximum and minimum outputs to obtain a series of calibration parameters;

fifth means coupled to said first means and said fourth means for applying said parameters to said time filtered outputs to convert said time filtered outputs from said first means to two winding outputs, said two windings being orthogonally related to one another;

sixth means for obtaining the calibrated compass heading from said two winding outputs.

2. The apparatus of claim 1 including seventh means coupled between said fifth means and said sixth means for normalizing said two winding outputs by dividing each of said two winding outputs by the square root of the sum of the squares of each of said two winding outputs.

3. The apparatus of claim 1 including eighth means coupled between each of said compass windings and each of said first means and said second means for sensing the amplitude of the winding outputs and increasing or decreasing the amplitudes of the winding outputs to fit within a predetermined sensor scale of amplitudes.

4. The apparatus of claim 3 wherein said eighth means comprises integrating means for integrating the winding incremental outputs and increasing the number of winding incremental outputs integrated when the winding outputs fall below the sensor scale and decreasing the number of winding incremental outputs integrated when the winding outputs are above the sensor scale.

5. The apparatus of claim 1 wherein the number of windings in the compass is three and the three windings are arcuately spaced approximately 120°

from one another and the outputs from the three windings are U, V, W respectively, said third means comprises computing means for obtaining ##EQU29## where B_u, B_v, B_w are biases and U, V, W are maximum outputs and U, V, W, are minimum outputs as the vehicle is turned through a complete circle;

said fourth means comprises computing means for obtaining ##EQU30##

6. The apparatus of claim 5 wherein the number of windings in the compass is three and the three windings are arcuately spaced 120°

from one another and the outputs from the three windings are U, V, W respectively, said first means comprises push down stack means for obtaining time filtered outputs U", V", W" having the form;

space="preserve" listing-type="equation">F=P.sub.1 -P.sub.2 -2P.sub.3 +4P.sub.4 -2P.sub.5 -P.sub.6 +P.sub.7

where for the U reading F=U"(t), P₁ =U(t), P₂ =V(t-1), P₃ =W(t-2), P₄ =U(t-3), P₅ =V(t-4), P₆ =W(t-5), P₇ =U(t-6);

where for the V reading F=V"(t), P₁ =V(t), P₂ =W(t-1), P₃ =U(t-2), P₄ =V(t-3), P₅ =W(t-4), P₆ =U(t-5), P₇ =V(t-6);

where for the W reading F=W"(t), P₁ =W(t), P₂ =U(t-1), P₃ =V(t-2), P₄ =W(t-3), P₅ =U(t-4), P₆ =V(t-5), P₇ =W(t-6) and where t=present time and (t-n) is the time equal to the present time t minus the next previous n time units.

7. The apparatus of claim 6 wherein said filtered outputs from said three windings are U", V", W" respectively and said two winding outputs are X, Y respectively, and said fifth means converts to the said two winding outputs by obtaining:

space="preserve" listing-type="equation">X=a.sub.11 (U"-B.sub.u)+a.sub.12 (V"-B.sub.v)+a.sub.13 (W"-B.sub.w)

space="preserve" listing-type="equation">Y=a.sub.21 (U"-B.sub.u)+a.sub.22 (V"-B.sub.v)+a.sub.23 (W"-B.sub.w).

8. The apparatus of claim 7 wherein said fifth means is for normalizing the X, Y outputs to obtain X'"'"', Y'"'"', respectively, as follows:

##EQU31##

9. The apparatus of claim 8 wherein said sixth means is for obtaining the heading arc tangent from X'"'"', Y'"'"'.

10. The apparatus of claim 1 wherein the number of windings in the compass is three and the three windings are arcuately spaced 120°

from one another and the outputs from the three windings are U, V, W respectively, said first means comprises push down stack means for obtaining time filtered outputs U", V", W" having the form;

space="preserve" listing-type="equation">F=P.sub.1 -P.sub.2 -2P.sub.3 +4P.sub.4 -2P.sub.5 -P.sub.6 +P.sub.7

where for the U reading F=U"(t), P₁ =U(t), P₂ =V(t-1), P₃ =W(t-2), P₄ =U(t-3), P₅ =V(t-4), P₆ =W(t-5), P₇ =U(t-6);

where for the V reading F=V"(t), P₁ =V(t), P₂ =W(t-1), P₃ =U(t-2), P₄ =V(t-3), P₅ =W(t-4), P₆ =U(t-5), P₇ =V(t-6);

where for the W reading F=W"(t), P₁ =W(t), P₂ =U(t-1), P₃ =V(t-2), P₄ =W(t-3), P₅ =U(t-4), P₆ =V(t-5), P₇ =W(t-6) and where t=present time and (t-n) is the time equal to the present time t minus the next previous n time units.

11. The apparatus of claim 10 wherein said filtered outputs from said three windings are U", V", W" respectively and said two winding outputs are X, Y respectively, and said fifth means converts to the said two winding outputs by obtaining:

space="preserve" listing-type="equation">X=a.sub.11 (U"-B.sub.u)+a.sub.12 (V"-B.sub.v)+a.sub.13 (W"-B.sub.w)

space="preserve" listing-type="equation">Y=a.sub.21 (U"-B.sub.u)+a.sub.22 (V"-B.sub.v)+a.sub.23 (W"-B.sub.w).

12. The apparatus of claim 11 wherein said fifth means is for normalizing the X, Y outputs to obtain X'"'"', Y'"'"', respectively, as follows:

##EQU32##

13. The apparatus of claim 12 wherein said sixth means is for obtaining the heading arc tangent from X'"'"', Y'"'"'.

14. Apparatus for calibrating the distortions in the readings of a magnetic compass having a plurality of separated vector outputs having a common origin and mounted in a vehicle comprising:

first means coupled to the compass for providing output terminals corresponding to each of said vector outputs;

second means coupled to said first means terminals for calibrating the compass vector outputs for distortions due to the permanent and induced magnetism of the vehicle and providing first distortion correction signals;

third means coupled to said first means terminals for calibrating the gain imbalance and separation misorientation between the vector outputs and providing second distortion correction signals;

fourth means coupled to said second and third means for receiving said first and second distortion correction signals and for providing a calibrated compass heading.

15. The apparatus of claim 14 wherein said second means comprises means for compensating for the origin offset due to the permanent magnetic distortion effect of the vehicle on the compass vector outputs, said offset being the difference between the vector origin location of the distorted vector outputs for all headings of the compass and the vector origin location of the undistorted vector outputs for all headings of the compass;

said second means further comprising means for compensating for the difference in configuration of geometric figures defined by the distorted vector outputs and the undistorted vector outputs due to the induced magnetic distortion effects of the vehicle on the compass vector outputs for all headings of the compass.

16. The apparatus of claim 15 wherein said geometric figure for the distorted vector outputs is in the shape of an ellipse and the geometric figure for the undistorted vector outputs is in the shape of a circle.

17. A method for calibrating the distortions in the readings of a magnetic compass having a plurality of windings in a two dimensional plane and mounted in a vehicle comprising the steps of:

first step of obtaining the outputs from each of the windings as a function of time by weighting and combining the outputs from each of the windings at a first time and for a predetermined number of the next previous times to said first time to obtain a time filtered output for each of the windings;

second step of receiving the time filtered outputs and for obtaining maximum and minimum filtered outputs for each of the windings as the vehicle is turned through a circle of 360°

;

third step of determining biases from the maximum and minimum filtered outputs equal to the average of the maximum and minimum filtered outputs from each winding;

fourth step of applying said biases to said maximum and minimum outputs to obtain a series of calibration parameters;

fifth step of applying said parameters to said time filtered outputs to convert said time filtered outputs from said first means to two winding outputs, said two windings being orthogonally related to one another;

sixth step of obtaining the calibrated compass heading from said two winding outputs.

18. The method of claim 17 including a seventh step of normalizing said two winding outputs by dividing each of said two winding outputs by the square root of the sum of the squares of each of said two winding outputs.

19. The method of claim 17 including an eighth step of sensing the amplitude of the winding outputs and increasing or decreasing the amplitudes of the winding outputs to fit within a predetermined sensor scale of amplitudes.

20. The method of claim 17 wherein said fifth step comprises normalizing the X, Y outputs to obtain X'"'"', Y'"'"', respectively, as follows:

##EQU33##

21. The method of claim 20 wherein said sixth step comprises obtaining the heading arc tangent from X'"'"', Y'"'"'.

22. A method for calibrating the distortions in the readings of a magnetic compass having a plurality of separated vector outputs having a common origin and mounted in a vehicle comprising the steps of:

first step of calibrating the compass vector outputs for distortions due to the permanent and induced magnetism of the vehicle and providing first distortion correction signals;

second step of calibrating the gain imbalance and separation misorientation between the vector outputs and providing second distortion correction signals;

third step of receiving said first and second distortion correction signals and for providing a calibrated compass heading.

23. The method of claim 22 wherein said first step comprises compensating for the origin offset due to the permanent magnetic distortion effect of the vehicle on the compass vector outputs, said offset being the difference between the vector origin location of the distorted vector outputs for all headings of the compass and the vector origin location of the undistorted vector outputs for all headings of the compass;

said first step further comprising compensating for the difference in configuration of geometric figures defined by the distorted vector outputs and the undistorted vector outputs due to the induced magnetic distortion effects of the vehicle on the compass vector outputs for all headings of the compass.

24. The method of claim 23 wherein said geometric figure for the distorted vector outputs is in the shape of an ellipse and the geometric figure for the undistorted vector outputs is in the shape of a circle.