CA1184376A - Electrical compass - Google Patents

Electrical compass

Info

Publication number
CA1184376A
CA1184376A CA000421732A CA421732A CA1184376A CA 1184376 A CA1184376 A CA 1184376A CA 000421732 A CA000421732 A CA 000421732A CA 421732 A CA421732 A CA 421732A CA 1184376 A CA1184376 A CA 1184376A
Authority
CA
Canada
Prior art keywords
flux
signals
signal
providing
frequency
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA000421732A
Other languages
French (fr)
Inventor
Jeffrey L. Franks
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Johnson Controls Interiors Technology Corp
Original Assignee
Prince Corp USA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Prince Corp USA filed Critical Prince Corp USA
Application granted granted Critical
Publication of CA1184376A publication Critical patent/CA1184376A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C17/00Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes
    • G01C17/02Magnetic compasses
    • G01C17/28Electromagnetic compasses
    • G01C17/30Earth-inductor compasses

Abstract

ELECTRICAL COMPASS
ABSTRACT OF THE DISCLOSURE
A magnetic field detecting system for use with a flux-gate sensor includes an oscillator, the output of which is applied to a digital bandpass filter and frequency divided and also applied to the sensor, and phase detectors such that the frequency and phase of the output signals from the flux-gate sensor have a predetermined relationship to the excitation signal. In one embodiment of the invention, the direction indicating output signals from the phase detectors are applied to a suitable interface circuit for a microprocessor which converts the signals to a digital format employed for application, to an alpha-type display for displaying the octal magnetic orientation of a vehicle.

Description

7~

BACKCROUND OF THE IN~ENTION
The present invention relates to compasses and, particularly, to an electrical circuit for processing signals from a flux-gate magnetic sensor used in a compass.
Compasses for vehicles such as automobiles, typically, are after-market items of a relati-vely basic mechanical design. Such compasses, typically, attach to the dashboard of the vehicle and are of inexpensive construction including a compass card suspended by a pin bearing and mounted within a housing. Usually, they will include some elemental form of adjustment or compensation mechanism such as movable magnets for adjusting the compass to north and south, depending on the geographical area of use of the vehicle.
The theory o-f operation of flux-gate magnetic sensors is well known and one application to the automotive environment is described in an article entitled "~agnetic Field Sensor and its Application to Automobiles" by Hisatsugu Itoh published on February 25-29, 1980 by the Society of Automotive Engineers, Inc. as SAE Technical Paper No. 800123. In the commercia' embodiment of this system, the bandpass filters incorporated to detect the second harmonic of the excitation input frequencies for the sensor must be critically tuned such that -the quadrature information can be accurately detected and subsequently employed to drive a display of the vehicle heading. Not only must the system, however, be critically tuned, the stability of the bandpass filter and its power supply must be designed to be swbstantially drift free in order to provide accurate in-formation to the phase detectors such 1 that accurate direction display results.
SUMMA~Y OF THE PRESENT INVENTION
In order to overcome the deficiencies of the prior art flux-gate sensor application in the automotive environ-ment, and to provide a more accurate and yet, more readily assembled and less expensive system, the system of the present invention incorporates a digitally controlled band-pass filter and synchronous phase detector both of which are frequency and phase locked to an oscillator also employed to excite the flux-gate sensor such that tuning free assembly and operation of the system results. ~agnetic field detecting systems embodying the present invention for use with a flux-gate sensor include an oscillator9 the output of which is applied to a digital bandpass filter and frequency divided and also applied to the sensor, and phase detectors such that the frequency and phase of the excitation signal bear a direct and predetermined relation-ship to the signal output signals from the flux-gate sensor.
In one embodiment of the invention, the direction indicating output signals are applied to a suitable inter-face circuit -for a microprocessor. The microprocessor converts the signals to a digital format employed for appli-cation, to an alpha-type display for displaying, for example, the octal magnetic orientation of a vehicle.
These and other features, objects and advantages of the present invention can best be understood by reference to the following description thereof together with the accompanying drawings in which:
~RIEF DESCRIPTION OF THE DRAWINGS
~ig. 1 is a fragmentary, top plan view of a rear~
view mirror for a vehicle shown partly broken away and
-2--7~

1 incorporating a flux-gate type magnetic sensor;
Fig. 2 is an electrical circuit diagram partly in block and schematic form showing a system embodying the present invention; and Fig. 3 is an electrical circuit diagram in schematic form showing details of a portion of -the circuit shown in Fig. 2.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
Referring initially to Figs. 1 and 2, a flux-gate type magnetic sensor 10 is mounted within the cylindrical barrel 20 forming a portion of the mounting assembly for a rearview mirror 12 of a vehicle. The rearview mirror 12 including its housing 13 can be of conventional construction and is coupled to the cylindrical barrel 20 by means of a front ball joint 14 coupled to housing 13 by means of a stem 15. Barrel 20 includes a conventional socket for captively ancl pivotally holding ball 14 therein. Similarly, a rear ball joint 16 including a stem 17 couples the opposite end of cylinder 20 to a mounting bracket 18, typically secured to the windshield o-f a vehicle by means of a corresponding mating bracket adhered to the wind-shield or by connection to the vehicle headliner, in some instances. Barrel 20 also includes a socket for captively and pivotally receiving ball 16 such that mirror 12 can be adjusted ~or rear vision by the vehicle operator.
Barrel 20 can be of conventional construction in terms of the sockets for receiving fore and a~t balls 1 and 16, respectively, however, the diameter o-~ the mid-section of the barrel 20 is slightly enlarged to receive the flux~gate sensor 10. Sensor 10 includes a toroidal core 11 having a generally rectangular cross-section, an 1 excitation winding 13 helically wound around core 11 and orthogonally aligned -first and second sensing windings 21 and 23, respectively, poled as shown by the dots in Fig. 2 and wound in orthogonal relationship to one another about the toroid as shown in Fig. 1 to provide orthogonally phased output signals of varying magnitude depending upon the sensed external or earth's magnetic field. Sensor 10 is secured within the non-ferro-magnetic barrel by a suitable bcnding or potting material 19 to be horizontal when the mirror is in a normal adjusted position. Also, the North-South winding 21 is aligned to be parallel to the longitudinal axis of the vehicle. Electrical leads from the windings 13, 21 and 23 are extended from barrel 20 by a suitable cable 27 extending between the sensor 10 and the associated electrical circuits shown in Figs. 2 and 3.
As shown in Fig. 2, the compass system includes an oscillator 25 which in the preferred embodiment is an R-C oscillator having an output frequency of approximately 80 kHz at output terminal 26 thereof. The output signal from oscillator 25 is applied to a counter circuit 30 providing 400 Hz at output terminal 31 which is applied to a driver amplifier 32 which subsequently applies the 400 Hz signals to excitation winding 13 of sensor 10 by means of conductors 33 and 35. Counter 30 also provides an 800 Hz signal at output terminal 36 which is applied to synchronous phase detector circuits 50 and 52. The output terminal 26 of oscillator 25 is also coupled to clock input terminals of digital bandpass filters 40 and 42. Filters 40 and 42 also include signal input terminals 45 and 47~ respectively coupled to one end o~ sensing coils 21 and 23, as shown in Fig. 2, with the remaining terminals of coils 21 and 23 1 commonly coupled to system ground as shown in Fig. 2. The output of bandpass filters ~0 and 42 are coupled to the input terminals of synchronous phase detectors 50 and 52 such that selected harmonic frequency signals, as described in greater detail below, are applied to each of the synchronous phase detectors which are actuated by an enabling signal from counter 30 via an enabling line 37 to apply positive and negative half-cycle sinusoidal signals received from sensing coils 21 and 23 through bandpass ilters 40 and 42 to inte-grating and inverting amplifier circuits 62 and 64. The closed loop gain o~ the system is controlled through a ~eed-back path including conductors 61 and 63 extending between integrating amplifier 64 and flux-gate sense winding 21 and integrator 62 and flux-gate sense winding 23, respectively.
At the output terminals 65 and 66 ofintegrators 64 and 62, respectively, there is thus provided DC varying signals el and e2, respectively, which respresent the direction infor-mation -from sensing coils 21 and 23. The amplitude and polarity of el and e2 varies with vehicle direction with respect to the earth's magnetic field. These DC varying signals are applied to a suitable interface circuit 70, including for example, suita.ble amplifiers and an AD converter for converting the DC slgnal in-formation to digital signals.
The microprocessor 80 includes associated R~ and ROM
memories with the ROM programmed to mathematically derive an output control signal in the form of the arc tangent of the ratio el to provide a digital output control signal applied to a display driver ci.rcuit 90 for alpha display 100 such that octant direction information can be displayed to the vehicle operator. The processing of signals el and e2 from integrator circuits 62 and 64 by a conventional 1 microprocessor and program to provide the tan~l el in a digital format for octant display of vehicle direction is entirely conventional. Having described the overall system~
a detailed description of the preferred electrical circuit for providing the direction signal information -from the flux-gate sensor is now presented in conjunc~ion with Fig. 3.
Referring to Fig. 3, oscillator 25 provides an essentially square wave output frequency of 80 kHz applied to the input of counter circuit 30 comprising, in the pre-ferred embodiment, series coupled counters 32, 34 and 38 each of which are commercially available integrated circuit chips having model numbers indicated thereon and each of which are coupled to the +V power supply foT receiving operating power as well as to a system ground indicated by the triangular symbol. A floating ground~ indicated by a conventional ground symbol, is also provided inasmuch as the system is adapted for vehicle use and only a positive battery supply is typically available. Accordingly, a power supply 110 provides both a system ground 112 and a floating ground 114 which is coupled to the junction of resistors 113 and 115 by an operational amplifier 116 for impedance isolation. Filter capacitor 117 by-passes resistor 115 while a similar capacitor 118 AC couples grounds 112 and 114. Capacitors 130 and 131 are coupled as shown to stabi-lize analog ground.
Counter circuit 34 divides the 80 kHz signals from oscillator 25 to 16 kHz signals applied to the input of counter 38 which divides the signals by ten to provide 1600 Hz signals which are subsequently applied to input terminals 13 and 3 o~ counter 39 with the later signal being applied through an inverter circuit 41. Counter 39 develops an ~ 6 1 800 Hz generally square wave output signal at pin 2 thereof and 400 ~Iz output signals of opposite polarity at pins 15 and 14 which are applied to the driver amplifier circuit 32 -for driving excitation coil 13 associated with the flux-gate sensor 10 such that the flux-gate core is driven into saturation. Capacitor 13' is in parallel with coil 13 to suppress radio frequency interference.
Driver amplifier 32 is a push-pull type amplifier having one current path consisting of the collector-to-emitter current path of a first NPN transistor 120 (driven ~y a positive going signal from terminal 15 of counter 39) through resistor 122, through excitation coil 13, a second resistor 124, and a PNP transis~or 126 biased in a con-ductive mode by an opposite polarity signal from output terminal 14 of counter 39. During alternate half cycle of operation, the current path is reversed and is provided by the collector-to-emitter current path of NPN transistor 128 through resistor 124, coil 13, resistor 122 and the emitter-to-collector current path of transistor 129 to system ground 112. Thus, coil 13 is excited at a fundamental frequency of 400 Hz and core 11 is driven into saturation by the current through power transistors 120, 126 and 128 and 129, respectively at this fundamental frequency.
As is known, the flux-gate sensor 10 operates by the earth's or other external magnetic field off-setting the hysteresis curve for second harmonic frequency signals depending on the orientation of the flux-gate sensor with respect to the earth's magnetic field. Thus, it is desired to detect and measure the polarity and magnitude of the second harmonic (i.e. 800 Hz) signals from detection coils 21 and 23 which are orthogonally related. In order to 1 synchronize the detection of the second harmonic frequency signals by phase detectors 50 and 52, the 80n Hz signals from counter 39 are applied to input terminals 13 and 6, respectively of the phase detectors as well as an inverted polarity 800 Hz signal applied through an inverter circuit 51 to terminals 5 and 12 9 respectively of the phase detectors 50 and 52.
The input signals applied to phase detectors 50 and 52, however, are first filtered by bandpass filters 40 and 42 to substantially eliminate (40 db suppression) all but the second order harmonic frequencies. This is achieved by applying the signals from coils 21 and 23 to the signal input terminals 5 and 16 of bandpass filters 40 and 42, respectively. Circuits 40 and 42 are each 1/2 of a commer-cially available National Semiconductor integrated circuit chip, model number MF-10, which is a switched capacitor sampled data filter driven by the 80 kHz clock oscillator 25 and having the RC components shown coupled to provide an amplifier gain of approximately 1000 and having a Q of 50 to substantially eliminate all but the second harmonic frequency information coupled by capacitors 43 and 44 to the input terminals of phase detectors 50 and 52. The phase detectors are synchronized in phase with this second harmonic infor-mation by the 800 Hz signal applied to their clock input terminals from counter 3g and inverter 51 such that signals are applied to output terminals 2 and 3 of detector 50 and 9 and 10 of detector 52 only during a precise and pre-determined phase relationship to the fundamental driving frequency of 400 Hz applied to driver amplifier 32. In practice, the 800 Hz signals applied to synchronize phase detectors 50 and 52 are off-set approximately 90 -from the
3~

1 fundamental driving frequency such that the transition from logic zero to logic one and back occur during the enable portion of the signals applied to detectors 50 and 52 at the second harmonic frequency. Since the phase detectors as well as the driver amplifier are locked to the clock oscillator 25 through the counter circuits, this precise and predetermined phase relationship can be selected and maintained to provide a maximum amplitude output signal from the phase detectors for a given output signal -from sensing coils 21 and 23 without the necessity of tuning. The inverted ou~put signals on pins 2, 3 and 9, 10, respectively, of detectors 50 and 52 are applied to opposite polarity inputs of operational amplifier 64 and 62 which serve as integrating circuits in conjunction with the feedback and integrating capacitors and resistors coupled as shown in Fig. 3 to provide DC output signals el and e2 at output terminals 65 and 66. Signals el and e2 indicate the direction of orientation of the flux-gate sensor with respect to earth~s magnetic field and, therefore, that of the vehicle in which the sensor is mounted. By providing signals e and e2, corresponding to the orthogonal coordinates of direction and each of which can have a positive or negative polarity relative to floating ground, all the information necessary for the vehicle heading is available in these two signals. As noted above, these analog signals are converted into a digital format and applied to a microprocessor for providing digital information to a display 100, as sh-own in Fig. 2.
With the system of the present invention, therefore, signal information from coils 21 and 23 are filtered and detected in synchronism with the drive frequency applied to g 1 excitation coil 13, therefore providing precise, predeter-mined orthogonally related signal information pertaining to the direction of orientation of the flux-gate sensor with respect to a magnetic field without the necessity of precisely tuning bandpass filters. The utilization of such a system also eliminates the need for providing a crystal control or extremely stable oscillator since the oscillator frequency is not critical. Various modifications to the preferred embodiment of the present invention can be made.
~hus, for example, the display 100 may be digital, as shown, or an analog type. If desired, the microprocessor can provide information other than the alpha information cor-responding to the octant headings (N, NE, E, SE, S SW, W, NW) and, for example, can display degree heading or other magnetic ~ield in-formation. The location of the sensor 10, although preferably shown in the barrel 20 of the rear-view mirror mounting assembly~ can be positioned at other locations although preferably in the headliner area remote from the dashboard of the vehicle.
These and other modifications to the preferred embodiment of the present invention will become apparent to those skilled in the art and fall within the spirit and scope of the present invention as defined by the appended claims.

- 10~

Claims

The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows.

A control circuit for use with an electrically operated magnetic field detector employing a flux-gate sensor comprising:
an oscillator for providing clock frequency output signals;
counter means coupled to said oscillator and responsive to said clock frequency signals therefrom for providing an excitation frequency signal for a flux-gate sensor and for providing a synchronization signal at a harmonic frequency of said excitation frequency;
bandpass filter means coupled to said oscillator and including means for receiving signal information from a flux-gate sensor and responsive to signal information and signals from said oscillator to provide signals at said harmonic frequency of said excitation frequency; and detection means coupled to said filter means and to said counter means and responsive to the synchronization signal and signals from said filter means for providing output signals representative of the orientation of a flux-gate sensor to an external magnetic field.

The circuit as defined in claim 1 wherein said bandpass filter means is a digital sampled data filter.

The circuit as defined in claim 2 wherein said harmonic frequency is the second harmonic.

The circuit as defined in claim 3 wherein said detection means includes digital phase detection means having a signal input coupled to the output of said bandpass filter and having clock input means coupled to said counter means for synchronizing the detection of signal information with said excitation frequency signal.

The circuit as defined in claim 4 wherein said detection means further includes integrating means having input means coupled to said phase detection means for providing an analog output signal therefrom.

The system as defined in claim 5 and further including circuit means coupled to said integrating means for providing a display of the orientation of a flux-gate sensor.

A vehicle compass system comprising:
a flux-gate magnetic sensor having excitation input and signal output terminals;
an oscillator for providing clock frequency output signals;
counter means coupled to said oscillator and responsive to said clock frequency signals therefrom for providing an excitation frequency signal applied to said excitation input of said flux-gate sensor and for providing a synchronization signal at a harmonic frequency of said excitation frequency;
bandpass filter means coupled to said oscillator and to said signal output terminals of said flux-gate sensor and responsive to signal information from said flux-gate sensor and signals from said oscillator to pass signals therethrough at said harmonic frequency of said excitation frequency;
detection means coupled to said filter means and to said counter means and responsive to the synchronization signal and signals from said filter means for providing output signals representative of the orientation of a vehicle in which said flux-gate sensor is installed; and display means coupled to said detection means and responsive to said output signals for displaying the orientation information.

The circuit as defined in claim 7 wherein said harmonic frequency is the second harmonic.

The circuit as defined in claim 8 wherein said bandpass filter means is a digital sampled data filter.

The circuit as defined in claim 9 wherein said detection means includes digital phase detection means having a signal input coupled to the output of said band-pass filter and having clock input means coupled to said counter means for synchronizing the detection of signal information with said excitation frequency signal.

The circuit as defined in claim 10 wherein said detection means further includes integrating means having input means coupled to said phase detection means for providing an analog output signal therefrom.

A control circuit for use with an electrically operated vehicle compass employing a flux-gate sensor comprising:
an oscillator for providing clock frequency output signals;
counter means coupled to said oscillator and responsive to said clock frequency signals therefrom for providing an excitation frequency signal for a flux-gate sensor and for providing a synchronization signal at a harmonic frequency of said excitation frequency;
digital sampled data bandpass filter means coupled to said oscillator and including means for receiving signal information from each signal output of a flux-gate sensor and responsive to signal information and signals from said oscillator to pass therethrough signals at substantially only said harmonic frequency of said excitation frequency;
and digital phase detection means coupled to said filter means and to said counter means and responsive to the synchronization signal and signals from said filter means for providing output signals representative of the orientation of a flux gate sensor.

The circuit as defined in claim 12 wherein said harmonic frequency is the second harmonic.

The circuit as defined in claim 13 and further including integrating means having input means coupled to said digital phase detection means for providing an analog output signal therefrom.

The system as defined in claim 14 and further including circuit means coupled to said integrating means for providing a display of the orientation of a flux-gate sensor.

The system as defined in claim 15 wherein said excitation frequency is about 400 Hz.
CA000421732A 1982-03-02 1983-02-16 Electrical compass Expired CA1184376A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/353,896 US4424631A (en) 1982-03-02 1982-03-02 Electrical compass
US353,896 1982-03-02

Publications (1)

Publication Number Publication Date
CA1184376A true CA1184376A (en) 1985-03-26

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Family Applications (1)

Application Number Title Priority Date Filing Date
CA000421732A Expired CA1184376A (en) 1982-03-02 1983-02-16 Electrical compass

Country Status (6)

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US (1) US4424631A (en)
EP (1) EP0087890B1 (en)
JP (2) JPS58161819A (en)
CA (1) CA1184376A (en)
DE (1) DE3380313D1 (en)
ES (1) ES520188A0 (en)

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Also Published As

Publication number Publication date
EP0087890A3 (en) 1986-03-26
ES8407577A1 (en) 1984-09-16
DE3380313D1 (en) 1989-09-07
US4424631A (en) 1984-01-10
ES520188A0 (en) 1984-09-16
JPH0559235U (en) 1993-08-06
EP0087890B1 (en) 1989-08-02
EP0087890A2 (en) 1983-09-07
JPS58161819A (en) 1983-09-26

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