Electronic compass

• US 5,924,212 A
• Filed: 10/06/1997
• Issued: 07/20/1999
• Est. Priority Date: 10/09/1996
• Status: Expired due to Fees

• Current Assignee: Donnelly Corporation (Magna International Incorporated)
• Original Assignee: Donnelly Corporation (Magna International Incorporated)
• Inventors: Domanski, Stanley J.
• Primary Examiner(s): BENNETT, GEORGE B
• Application Number:
  US08/944,360
• Time in Patent Office: 652 Days
• Field of Search: 33/355 R, 33/356, 33/357, 33/361, 324/247, 324/253, 324/260
• US Class Current: 33/355.00R
• CPC Class Codes: G01C 17/30 Earth-inductor compasses
• CPC Class Codes: G01R 33/02 Measuring direction or magnitude of magnetic fields or magnetic flux G01R33/20 takes precedence

Abstract

An electronic compass includes at least two coil assemblies. Each coil assembly has a magnetic axis which is oriented at a known angle to that of the other coil. Each coil assembly has a pair of substantially identical coils having magnetic axes that are parallel in a reverse sense. The compass further includes an oscillator which oscillates at a frequency which is dependent upon the inductances of the coils. A current source causes current to flow in the coils and a switch alternately couples the current source to each of the coils of the coil assemblies. A processor analyzes the frequencies of oscillation of the oscillator when each of the coil assemblies is coupled to the current source in order to compute geographic orientation based upon the analysis.

Claims

1. An electronic compass comprising:

at least two coil assemblies having magnetic axes which are oriented at a known angle to each other, each said coil assembly having at least a pair of substantially identical coils having magnetic axes that are parallel in a reverse sense, each of said coils having an inductance which varies as a function of the strength of a magnetic field in which it is positioned;

at least one oscillator having frequencies of oscillation which are at least partially dependent upon the inductances of said coils;

a coil bias current source which causes current to flow in said coils;

at least one switch which alternatingly couples said coil bias current source to each of said coils of said coil assemblies; and

,

a processor electrically coupled to said at least one switch which analyzes said frequencies of oscillation of said at least one oscillator when each of said coils of said coil assemblies is coupled to said coil bias current source and computes geographic orientation based upon said analysis.

2. The electronic compass of claim 1 wherein each of said coil assemblies includes a magnetically permeable core, having a permeability which varies according to the strength of an externally applied magnetic field.

3. The electronic compass of claim 2 wherein each of said coil assemblies is wound on a bobbin having a hollow core, and each said magnetically permeable core is aligned with said magnetic axes of one of said coil assemblies and positioned inside said hollow core of said bobbin.

4. The electronic compass of claim 1 wherein said coils of said coil assemblies have a capacitance which, in combination with said inductance of said coils, substantially determines said frequency of oscillation of said oscillator.

5. The electronic compass of claim 1 wherein said coil bias current source is a constant current source.

6. The electronic compass of claim 1 wherein said at least one switch includes at least four transistors electrically coupled between said coils and said constant current source, said at least four transistors controlled by said processor.

7. The electronic compass of claim 6 wherein each of said at least four transistors is electrically coupled to one of said coils of said at least two coil assemblies, each of said bases of said at least four transistors is electrically coupled to said processor and each of said emitters of said at least four transistors is electrically coupled to a common node.

8. The electronic compass of claim 7 wherein said common node is connected to said constant current source.

9. The electronic compass of claim 1 further including a display electrically coupled to said processor, said display producing a visibly readable output showing the geographic orientation of the compass.

10. The electronic compass of claim 9 wherein said display is a compass mirror.

11. The electronic compass of claim 2 wherein said magnetically permeable cores are plates.

12. The electronic compass of claim 10 wherein said plates have rectangular cross-sections.

13. The electronic compass of claim 2 wherein said magnetically permeable cores have a direct current relative permeability of greater than approximately 80,000.

14. The electronic compass of claim 5 wherein said constant current source includes an operational amplifier, a MOSFET, a sense voltage, and a reference voltage, said sense voltage is fed to a non-inverting input of said operational amplifier where said voltage is subsequently servoed to said reference voltage and said MOSFET adjusts itself to maintain said sense voltage.

15. The electronic compass of claim 1 wherein said oscillator is an LC oscillator.

16. The electronic compass of claim 1 wherein said processor computes geographic orientation by calculating the arctangent of the ratio of the difference in frequencies of oscillation between said pair of substantially identical coils in one of said coil assemblies and the difference in frequencies of oscillation between said pair of substantially identical coils in another of said coil assemblies.

17. The electronic compass of claim 1 wherein said processor stores values corresponding to the maximum and minimum frequency differences between said substantially identical coils for each coil assembly as said compass is incrementally rotated 360 degrees during a calibration sequence.

18. The electronic compass of claim 1 wherein said processor executes an algorithm which removes from the computed geographic orientation inaccuracies generated by an ambient, non-Earth magnetic field.

19. An electronic compass, comprising:

at least two coil assemblies wound around magnetically permeable cores, said coil assemblies having magnetic axes which are oriented at a known angle to each other, said coil assemblies having inductances, and said coil assemblies each comprising bifilar wound coils;

at least one oscillator having frequencies of oscillation which are at least partially dependent upon the inductances of said coil assemblies;

a constant current source which causes current to flow in said coils of said coil assemblies;

at least one switch which alternatingly couples said constant current source to each of said coils of said coil assemblies so as to allow current from said constant current source to alternatingly flow through each of said bifilar wound coils of said coil assemblies; and

,

a processor electrically coupled to said at least one switch which controls said switch and which compares said frequency of oscillation of said at least one oscillator when each of said coils of said coil assemblies is coupled to said constant current source and computes geographic orientation based upon said comparison.

20. The electronic compass of claim 19 wherein said magnetically permeable cores, have a permeability which varies according to the strength of an externally applied magnetic field.

21. The electronic compass of claim 20 wherein each of said coil assemblies is wound on a bobbin having a hollow core, and each said magnetically permeable core is aligned with said magnetic axes of one of said coil assemblies and positioned inside said hollow core of said bobbins.

22. The electronic compass of claim 20 wherein said bifilar wound coils of said coil assemblies have a capacitance which, in combination with said inductance of said coils, substantially determines said frequency of oscillation of said oscillator.

23. The electronic compass of claim 20 wherein said at least one switch includes at least four transistors electrically coupled between said coils and said constant current source, said at least four transistors controlled by said processor.

24. The electronic compass of claim 23 wherein each of said at least four transistors is electrically coupled to one of said coils of said at least two coil assemblies, each of said bases of said at least four transistors is electrically coupled to said processor and each of said emitters of said at least four transistors is electrically coupled to a common node.

25. The electronic compass of claim 24 wherein said common node is connected to said constant current source.

26. The electronic compass of claim 20 further including a display electrically coupled to said processor, said display producing a visibly readable output showing the geographic orientation of the compass.

27. The electronic compass of claim 20 wherein said display is a compass mirror.

28. The electronic compass of claim 20 wherein said magnetically permeable cores are plates having rectangular cross-sections.

29. The electronic compass of claim 20 wherein said magnetically permeable cores have a direct current relative permeability of greater than approximately 80,000.

30. The electronic compass of claim 20 wherein said constant current source includes an operational amplifier, a MOSFET, a sense voltage, and a reference voltage, said sense voltage is fed to a non-inverting input of said operational amplifier where said voltage is subsequently servoed to said reference voltage and said MOSFET adjusts itself to maintain said sense voltage.

31. The electronic compass of claim 20 wherein said oscillator is an LC oscillator.

32. The electronic compass of claim 20 wherein said processor computes geographic orientation by calculating the arctangent of the ratio of the difference in frequencies of oscillation between said pair of substantially identical coils in one of said coil assemblies and the difference in frequencies of oscillation between said pair of substantially identical coils in another of said coil assemblies.

33. The electronic compass of claim 20 wherein said processor stores values corresponding to the maximum and minimum frequency differences between said substantially identical coils for each coil assembly as said compass is incrementally rotated 360 degrees during a calibration sequence.

34. The electronic compass of claim 20 wherein said processor executes an algorithm which removes from the computed geographic orientation inaccuracies generated by an ambient, non-Earth magnetic field.

35. A method for electronically determining geographic orientation comprising the steps of:

providing at least two coil assemblies each having a magnetically permeable core, each said coil assembly having two substantially identical bifilar wound coils having magnetic axes that are collinear but oppositely oriented, and each of said two substantially identical bifilar wound coils having an inductance which varies as a function of the strength of an externally applied magnetic field;

providing an oscillator having a frequency of oscillation which is at least partially determined by said inductance of said coils;

alternatingly inducing a current in each of said coils while monitoring the frequency of oscillation of said oscillator; and

calculating heading from the frequency of oscillation of said oscillator when said current is induced in each of said coils.

36. The method of claim 35 wherein said step of calculating heading further includes the steps of:

computing a first difference between said frequencies of oscillation of said oscillator when current is induced in each of said two coils of one of said at least two coil assemblies;

computing a second difference between said frequencies of oscillation of said oscillator when current is induced in each of said two coils of another of said at least two coil assemblies; and

computing the arctangents of the ratio of said first and said second differences.

37. The method of claim 36 further including the steps of selecting one of said arctangents based on whether said first difference is positive or negative and whether said second difference is positive or negative.

38. The method of claim 35 further including a calibration step consisting of:

incrementally rotating said at least two coil assemblies through one revolution;

generating a first series of data by computing a first difference between said frequencies of oscillation of said oscillator when current is induced in each of said two coils of one of said at least two coil assemblies for each increment of rotation;

generating a second series of data by computing a second difference between said frequencies of oscillation of said oscillator when current is induced in each of said two coils of another of said at least two coil assemblies;

selecting a maximum and minimum first difference from said first series of data;

calculating a first calibration number by summing said maximum and said minimum first differences and dividing the sum by two;

selecting a maximum and minimum second difference from said second series of data; and

calculating a second calibration number by summing said maximum and said minimum second differences and dividing the sum by two.

39. The method of claim 38 further including the steps of:

computing a first difference between said frequencies of oscillation of said oscillator when current is induced in each of said two coils of one of said at least two coil assemblies;

computing a second difference between said frequencies of oscillation of said oscillator when current is induced in each of said two coils of another of said at least two coil assemblies;

subtracting said first calibration number from said first difference to yield a first result;

subtracting said second calibration number from said second difference to yield a second result; and

computing the arctangents of a ratio of said first and second results.

40. The method of claim 39 further including the steps of selecting one of said arctangents based on whether said first result is positive or negative and whether said second result is positive or negative.

41. An electronic compass, comprising:

at least two coils axially oriented at a known angle to each other, said at least two coils having inductances;

at least one oscillator having frequencies of oscillation which are at least partially dependent upon said inductances of said at least two coils;

a constant current source which causes current to flow in said coils of said coil assemblies;

at least one switch which alternatingly couples said constant current source to each of said at least two coils as to allow current from said constant current source to alternatingly flow through each of said at least two coils; and

,

a processor which analyzes said frequencies of oscillation of said at least one oscillator when each of said coils is coupled to said constant current source and computes geographic orientation based upon said analysis.