Method and apparatus for automatic calibration of magnetic compass

• US 4,797,841 A
• Filed: 07/02/1986
• Issued: 01/10/1989
• 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.
• Primary Examiner(s): Gruber, Felix D.
• Application Number:
  US06/881,441
• Time in Patent Office: 923 Days
• Field of Search: 364/571, 364/556, 364/559, 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; the filtered outputs are mapped into equivalent two winding outputs as the vehicle is turned in a 360° circle to form sensitivity values from the windings readings and using these values to obtain measurement parameters which are incorporated into a least squares matrix which is solved for calibration coefficients to obtain the calibration parameters representing the distortions due to the permanent and inducted magnetism of the host vehicle and due to winding imbalance between the three windings and misorientation of the three windings. The calibration parameters 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 to form from said windings outputs measurement parameters having sensitivity values;

said sensitivity values being variables in a generalized equation that represents the configuration and location of a geometrical figure defined by the locus of coordinates of said outputs, said outputs having distortions due to permanent and induced magnetism of the vehicle and distortions due to winding imbalance between the misorientation of the magnetic compass windings;

said second means for defining calibration coefficients of said measurement parameters in said equation;

third means coupled to said second means to incorporate said measurement parameters and said calibration coefficients into a least squares matrix and to solve for said calibration coefficients;

fourth means coupled to said third means for computing calibration parameters from said calibration coefficients that are to be applied to said outputs;

fifth means coupled to said first means and said fourth means for applying said calibration parameters to said outputs from said first means to form an output from each of two windings;

said two windings being orthogonally related to one another;

sixth means coupled to said fifth means for obtaining the calibrated compass heading from said two windings outputs.

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

said generalized equation in said second means being;

space="preserve" listing-type="equation">x.sup.2 +y.sup.2 =b.sub.1 +b.sub.2 (x.sup.2 -y.sup.2)+b.sub.3 (-2xy)+b.sub.4 (2x)+b.sub.5 (2y)

in said second means said measurement parameters being m_o, m₁, m₂, m₃, m₄, m₅ and having having the sensitivity values x² +y², 1, x² -y², -2xy, 2x and 2y, respectively;

in said second means said calibration coefficients comprise;

b₁ =[a₁ -(1-a₂)x_o² -(1+a₂)y_o² -2a₃ x_o y_o ]

b₂ =a₂

b₃ =a₃

b₄ =[(1-a₂)x_o +a₃ y_o ]

b₅ =[(1+a₂)y_o +a₃ x_o ]

where

a₁ =2b² /(2-e²)

a₂ =e² C₂ /(2-e²)

a₃ =e² S₂ /(2-e²)

a=semimajor axis of ellipse

b=semiminor axis of ellipse ##EQU38## C₂ =cosine (2θ

) and S₂ =sine (2θ

) θ

=rotation angle of ellipse

x,y=coordinates of center of ellipse prior to offset

x_o,y_o =coordinates of offset center of ellipse

said least squares matrix in said third means comprises;

##EQU39## where the matrix [Σ

(M^T M)]^-1 is the inverse of the matrix Σ

(M^T M)

said calibration parameters in said fourth means comprise;

##EQU40##

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:

##EQU41##

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:

##EQU42##

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

15. The method of claim 4 wherein said first step comprises 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;

14. 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:

a first step of obtaining the outputs from each of the windings;

a second step of forming from said windings outputs measurement parameters having sensitivity values;

said sensitivity values being variables in a generalized equation that represents the configuration and location of a geometrical figure defined by the locus of coordinates of said outputs, said outputs having distortions due to permanent and induced magnetism of the vehicle and distortions due to winding imbalance between and misorientation of the magnetic compass windings;

said second step defining calibration coefficients of said measurement parameters in said equation;

a third step of incorporating said measurement parameters and said calibration coefficients into a least squares matrix and solving for said calibration coefficients;

a fourth step of computing calibration parameters from said calibration coefficients that are to be applied to said outputs;

a fifth step of applying said calibration parameters to said outputs from said first step to form an output from each of two windings;

said two windings being orthogonally related to one another;

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

16. The method of claim 14 including a seventh step of normalizing said two windings outputs by dividing each of said two windings outputs by the square root of the sum of the squares of each of said two windings outputs.

17. The method of claim 14 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.

18. The method of claim 17 wherein said eighth step comprises 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, to fit the outputs within a predetermined sensor scale of amplitudes.

19. The method of claim 14 wherein said geometrical 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;

said generalized equation being;

space="preserve" listing-type="equation">x.sup.2 +y.sup.2 =b.sub.1 b.sub.2 (x.sup.2 -y.sup.2)+b.sub.3 (-2xy)+b.sub.4 (2x)+b.sub.5 (2y)

said measurement parameters being m_o, m₁, m₂, m₃, m₄, m₅ and having the sensitivity values x² +y², 1, x² -y², -2xy, 2x and 2y, respectively;

said calibration coefficients comprise;

b₁ =[a₁ -(1-a₂)x_o² -(1+a₂)y_o² -2a₃ x_o y_o ]

b₂ =a₂

b₃ =a₃

b₄ =[(1-a₂)x_o +a₃ y_o ]

b₅ =[(1+a₂)y_o +a₃ x_o ]

where

a₁ =2b² /(2-e²)

a₂ =e² C₂ /(2-e²)

a₃ =e² S₂ /(2-e²)

a=semimajor axis of ellipse

b=semiminor axis of ellipse ##EQU43## C₂ =cosine (2θ

) and S₂ =sine (2θ

) θ

=rotation angle of ellipse

x,y=coordinates of center of ellipse prior to offset

x_o,y_o =coordinates of offset center of ellipse

said least squares matrix comprises;

##EQU44## where the matrix [(M^T M)]^-1 is the inverse of the matrix Σ

(M^T M)

said calibration parameters comprise;

##EQU45##

20. The method of claim 14 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.

21. 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;

second means coupled to said first means to form from said windings outputs measurement parameters having sensitivity values;

said sensitivity values being variables in a generalized equation that represents the configuration and location of a geometrical figure defined by the locus of coordinates of said outputs, said outputs having distortions due to permanent and induced magnetism of the vehicle and distortions due to winding imbalance between and misorientation of the magnetic compass windings;

said second means for defining calibration coefficients of said measurement parameters in said equation;

third means coupled to said second means to incorporate said measurement parameters and said calibration coefficients into a least squares matrix and to solve for said calibration coefficients;

fourth means coupled to said third means for computing calibration parameters from said calibration coefficients that are to be applied to said outputs;

fifth means coupled to said first means and said fourth means for applying said calibration parameters to said outputs from said first means to form an output from each of two windings;

said two windings being orthogonally related to one another;

sixth means coupled to said fifth means for obtaining the calibrated compass heading from said two windings outputs.