Flux-gate sensor mounting and method

• US 5,253,424 A
• Filed: 12/27/1991
• Issued: 10/19/1993
• Est. Priority Date: 12/27/1991
• Status: Expired due to Fees

• Current Assignee: Chrysler Corporation (Stellantis NV)
• Original Assignee: Chrysler Corporation (Stellantis NV)
• Inventors: Kendall, Jeffrey M.
• Primary Examiner(s): Cuchlinski, Jr., William A.
• Assistant Examiner(s): FULTON, CHRISTOPHER W
• Application Number:
  US07/815,265
• Time in Patent Office: 662 Days
• Field of Search: 33/355 R, 33/361, 33/356, 33/357, 33/358
• US Class Current: 33/361
• CPC Class Codes: G01C 17/30 Earth-inductor compasses

Abstract

A flux-gate sensor orientation method which minimizes display jitter in electronic compasses which employ an n-point display or which calculate headings using the arctangent method. The method entails orienting the flux-gate sensor in a direction of plus or minus ±360°/2n relative to actual magnetic direction, so that instability points occur at display point boundaries. The method of the present invention finds application in microprocessor-based electronic compass systems but also makes possible the construction of a simple electronic compass employing small scale integration logic instead of a microprocessor.

Claims

1. In an electronic compass system, including a flux-gate sensor having first and second orthogonal sense coils, said electronic compass using the arctangent function to calculate headings and displaying n sectors having n boundaries separated by a fixed number of degrees, wherein said boundaries are offset with respect to actual magnetic directions, a method of orienting a flux-gate sensor relative to actual magnetic directions to minimize display jitter between the boundaries, said method comprising:

(a) orienting the display with actual magnetic directions; and

(b) orienting the first and second sense coils along four of said boundaries.

2. The method as recited in claim 1, further comprising:

(c) generating a logic table having a plurality of values, each said value of the logic table being associated with a sector; and

(d) determining compass headings from said logic table.

3. The method as recited in claim 1 wherein step (b) comprises orienting the first sense coil plus or minus ±

360°

/2n degrees relative to actual magnetic directions.

4. The method as recited in claim 3, wherein for n=8, the first sense coil is orientated ±

22.5°

relative to actual magnetic directions.

5. An electronic compass system for use in areas far enough from ferrous metals so as to be unaffected by the magnetic fields associated with such metals, comprising:

(a) a flux-gate sensor having perpendicular first and second sense coils, each said sense coil being operable to generate a signal thereacross;

(b) first circuit means for conditioning and processing the signal across the first sense coil and for producing a first direct current output signal;

(c) second circuit means for conditioning and processing the signal across the second sense coil and for producing a second direct current output signal;

(d) logic means, coupled to said first and second circuit means and having an output for determining compass heading using said first and second direct current output signals;

(e) display interface means coupled to said logic means for converting the output of said logic means to a signal for display; and

(f) display means coupled to said display interface means for displaying compass headings, said display means being divided into n sectors having n boundaries separated by a fixed number of degrees, wherein said boundaries are offset with respect to actual magnetic directions;

said first and second sense coils being oriented along four of said sector boundaries.

6. The electronic compass system of claim 5 wherein said first sense coil is oriented plus or minus ±

360°

/2n relative to actual magnetic direction.

7. The electronic compass system of claim 5 wherein said logic means comprises:

(a) a first comparator for comparing the first direct current output signal from the first circuit means with a reference signal and for producing an output signal indicative of the polarity of the first direct output signal;

(b) a second comparator for comparing the second direct current output signal with the reference signal and for producing an output signal indicative of the polarity of the second direct current output signal; and

(c) a third comparator for comparing the magnitude of the first direct current output signal with the magnitude of the second direct current output signal and for producing an output indicative of the relative magnitudes of the first direct current output signal and the second direct current output signal.

8. The electronic compass system of claim 7 wherein said logic means further comprises:

(d) a first Schmitt Trigger for delaying the first comparator output signal by a half-cycle;

(e) a second Schmitt Trigger for delaying the second comparator output signal by a half-cycle;

(f) first inverter means coupled to said first circuit means for inverting the first direct output signal and generating an output signal representative thereof;

(g) second inverting means coupled to said second circuit means for inverting the second direct output signal and generating an output signal representative thereof;

(h) a quad bilateral switch having four switches, the first switch being coupled to the first direct output signal and clocked by said first comparator output signal, the second switch being coupled to the output signal of the first inverting means and clocked by said first Schmitt Trigger output signal, the third switch being coupled to the second direct output signal and clocked by said second comparator output signal, and the fourth switch being coupled to the output signal of the second inverting means and clocked by said second Schmitt Trigger output signal, the first and second switch outputs being coupled to thereby produce a full-wave rectified first direct output signal coupled to said third comparator, and said third and fourth switch outputs being coupled to thereby produce a full-wave rectified second direct output signal to said third comparator.

9. The electronic compass system of claim 5 wherein said display means comprises a compass rose and n light-emitting diodes, one for each of the n sectors.

10. The electronic compass system of claim 9 wherein said display means comprises eight light-emitting diodes.

11. The electronic compass system of claim 5 wherein said display interface logic means comprises an octal decoder.

12. An electronic compass system for determining vehicle headings comprising:

(a) a flux-gate sensor, having first and second orthogonal sense coils, said flux-gate sensor being oriented plus or minus ±

360°

/2n relative to actual magnetic directions;

(b) signal processing means coupled to said flux-gate sensor for generating first and second output signals having information about the heading of the vehicle; and

(c) logic means responsive to said signal processing means for determining vehicle headings.