GB2151790A - Hall effect transmitting compass - Google Patents

Hall effect transmitting compass Download PDF

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Publication number
GB2151790A
GB2151790A GB08333814A GB8333814A GB2151790A GB 2151790 A GB2151790 A GB 2151790A GB 08333814 A GB08333814 A GB 08333814A GB 8333814 A GB8333814 A GB 8333814A GB 2151790 A GB2151790 A GB 2151790A
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GB
United Kingdom
Prior art keywords
sensors
hall effect
compass
casing
pair
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.)
Withdrawn
Application number
GB08333814A
Inventor
Vincent Philip May
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.)
TIMELOCK Ltd
Original Assignee
TIMELOCK Ltd
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 TIMELOCK Ltd filed Critical TIMELOCK Ltd
Priority to GB08333814A priority Critical patent/GB2151790A/en
Publication of GB2151790A publication Critical patent/GB2151790A/en
Withdrawn legal-status Critical Current

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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

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  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Electromagnetism (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Or Calibration Of Command Recording Devices (AREA)

Abstract

A Hall effect transmitting compass comprises a ring magnet (1) which is pivotally mounted in an oil-filled chamber of casing (7) and at least one pair of Hall effect sensors (11) mounted on the casing in the plane of the ring magnet when said magnet is horizontal. The sensors (11) are connected by electric leads (15) to an electric circuit on a printed circuit board (12) secured by screws (13) to the casing (7). The circuit, described in detail, evaluates signals from the sensors and provides an output from which a compass heading of the ring magnet can be determined. One pair of Hall effect sensors is preferred for use in automatic pilot systems, whereas two pairs are needed to obtain an unambiguous directional signal. <IMAGE>

Description

SPECIFICATION Hall effect transmitting compass This invention relates to an electronic transmitting compass.
Transmitting compasses are well-known and widely used pieces of equipment both as navigational aids and as control sensors for other equipment such as automatic pilots.
Transmitting compasses currently available fall into three major categories: i) The flux gate compass: This compass is a completely solid state device with no moving parts which derives a heading by sensing the direction of the lines of magnetic flux generated by the earth's natural magnetic pole.
ii) The optical pick-up compass: This compass uses a conventional magnetic movement with a specially prepared card. A heading is derived by shining light through the special card onto a light dependant resistor or photo-diode.
iii) The coil sensing compass: This compass uses three coils connected in a star formation mounted above or below a conventional magnetic compass.
A fourth coil is used as an exciter at high frequency and hence the output from the three other coils can be decoded to determine the exact position of the magnet in the compass.
All three types of compass suffer from the same inherent fault; they are all very sensitive to tilt i.e.
they will all return an incorrect heading if the compass housing is tilted by as little as 3 -5 . In order to overcome this problem these compasses are usually mounted in an elaborate gimball system however, due to friction and inertia, errors still occur.
The present invention aims to provide a compass which avoids the disadvantages of the known compasses discussed above.
According to the invention, there is provided a Hall effect transmitting compass comprising a ring magnet pivotally mounted in an oil-filled chamber of a casing and at least one pair of Hall effect sensors mounted on or in close proximity to the casing in the plane of said ring magnet when said magnet is horizontal, said sensors serving to sense the position of the magnet.
Preferably, the sensors are mounted at diametri cally opposite locations one the casing whereby said sensors are spaced apart by 1800. If the sensors were mounted below or above the magnet then the output would be no better than that of any of the three conventional transmitting compass designs discussed above because as the magnet tilted, it would be nearer to one sensor than the other and so return a false reading. By locating the sensors in the same plane as the ring magnet when the latter is horizontal, and positioning two Hall effect sensors at the edge of the ring magnet at 1800 to each other, accurate readings over 1800 of compass movement can be obtained and would find application in control mechanisms such as an automatic pilot.
In order to return accurate readings over a full 360" a second pair of sensors must be fitted at 90" to the original pair. Thus, according to a preferred embodiment of the invention, a second pair of Hall effect sensors is mounted on or in close proximity to the casing in the same plane as said first pair of sensors.
The sensors of the second pair are desirably mounted at diametrically opposite locations on the casing whereby said second pair of sensors are spaced apart from each other by 1800 and adjacent sensors are spaced apart from each other by 90".
The Hall effect sensors are desirably connected to a circuit for evaluating values sensed by the sensors and for giving an indication of the associated compass heading.
This configuration renders the compass completely immune from any tilt error as only the two sensors that are positioned opposite each other (at 1800 spacing) are read at any one instant in time and hence no matter what angle the magnet is tilting at, it is always the same distance away from the two 'live' sensors.
The invention will now be further described, by way of example, with reference to the drawings, in which: Figure 1 is a part-sectional plan view of one embodiment of a compass according to the invention; Figure 2 is a section taken on the line ll-ll of Figure 1; Figure 3 is a circuit diagram of a compass according to the invention having two Hall effect devices; Figure 4 is a graph showing the output curves produced by the circuit shown in Figure 3; Figure 5 is a circuit diagram of a compass according to the invention having four Hall effect devices and a channel selector; and Figure 6 is a graph showing the output curves produced by the circuit shown in Figure 5.
Reference will first be made to Figures 1 and 2 of the drawings in which the compass comprises a conventional ring magnet 1 to which a peripheral flange 2 of a dome 3 is secured. The dome 3 carries on its lower, concave, face a pivot pin 4 which is pivotally mounted in a jewelled bearing 5 mounted on a screw-threaded pin 6 which is secured to the base of a casing 7. The ring magnet 1 and a dome 3 are mounted for pivotal movement in the casing 7 which is filled with oil in order to damp pivoting movements of the magnet. The magnet is free to tilt up to 300 in any direction and it will be noted that no compass card is provided.
The casing 7 is desirably made of plastics material and is closed at the top by a cover 8 which prevents the escape of oil from the casing. The cover is provided with a splined sleeve 9 for the reception of knob (not shown). The cover 8 and sleeve 9 have been omitted from Figure 1 in the interests of clarity.
Positioned on diametrically opposite sides of the casing, at 1800 to each other respectively, are two Hall effect sensors 11. In the embodiment shown in Figure 2, two pairs of Hall effect sensors are provided, adjacent sensors being spaced from each other by 90" and diametrically opposite sensors constituting each respective pair. However, as will be explained later, it is possible to provide only one pair of Hall effect sensors for some uses of the compass according to the invention.
The Hall effect sensors 11 are positioned on the sides of the casing 7 at the same time horizontal level as the ring magnet 1 when said magnet is horizontal. A small printed circuit board 12 is secured by screws 13 to pillars 14 extending from the base of the casing 7 and is electrically connected to the Hall effect sensors 11 by electric leads 15.
Turning now to Figure 3, the circuit comprises two of the Hall effect sensors 11, which are positioned respectively at East and West locations and are connected in the manner shown in this drawing.
The output from the sensor 11 located in the West position is fed, via a setting resistor VR2 and an impedance matching resistor R2, into the inverting input of a first amplifer AMP1. The output level of this Hall effect sensor is set at 3 volts by adjusting the resistor VR2 at zero magnetic flux density.
The output from the sensor 11 located in the East position is fed, via a setting resistor VR1 and an impedance matching resistor R1 into the noninverting input of the first amplifier AMP1. The output of this amplifier is now set to 0.10 volts by adjusting the resistor VR1 at zero magnetic flux density.
The output from the amplifier AMP1 is now fed into the non-inverting input of a second amplifier AMP2 which is adjusted by a setting resistor VR3 to give an output of 2.5 volts at zero magnetic flux density.
Figure 4 shows voltage output against compass heading. It can be seen that for any given voltage it is possible to derive two different headings of 1800 ambiguity. This feature makes this compass ideal for use in applications such as automatic pilots where the compass itself is turned to set the desired steering course. The 1800 ambiguity is desirable to allow for port or starboard mounting of tiller accuators without any changes at all to the circuitry.
The compass housing is pointing directly north or south when a voltage output of 2.5 volts is achieved.
Figure 5 shows the circuitry for a 360" version having four Hall effect sensors 11. Each pair of sensors is arranged in a circuit having the same configuration as the 1800 version shown in Figure 3 but arranged as two separate channels which can be individually selected by a master control unit 16 by using the two address line Ao and Al. By selecting first one channel and then the other, two values can be obtained which when integrated will give a unique position between 1 and 360".
Figure 6 shows voltage output against compass heading for both channels on the 360 version. It can be seen that for any heading there is always a unique combination of voltage outputs on channel 1 and 2 and hence a fully proportional and accurate heading can be derived from the two outputs by the master control unit.
It will be seen that, by means of the invention, it is possible to provide a Hall effect transmitting compass which is immune from tilt error without the need for gimballing. The output can be set to cover just 1800 of magnet movement or by duplicating the basic configuration can be set to cover the full 360" of magnet movement. The compass can therefore be used for either simple automatic pilot control in its 1800 mode or as a full repeater compass or large ship automatic pilot control in its 360" mode.

Claims (6)

1. A Hall effect transmitting compass comprising a ring magnet pivotally mounted in an oil-filled chamber of a casing and at least one pair of Hall effect sensors mounted on or in close proximity to the casing in the plane of said ring magnet when said magnet is horizontal, said sensors serving to sense the position of magnet.
2. A Hall effect transmitting compass according to claim 1, wherein said sensors are mounted at diametrically opposite locations on the casing whereby said sensors are spaced apart by 1800.
3. A Hall effect transmitting compass according to claim 1 or claim 2, wherein a second pair of Hall effect sensors is mounted on or in close proximity to the casing in the same plane as said first pair of sensors.
4. A Hall effect transmitting compass according to claim 2 and claim 3, wherein the sensors of said second pair are mounted at diametrically opposite locations on the casing whereby said second pair of sensors are spaced apart from each other by 180 and adjacent sensors are spaced apart from each other by 90".
5. A Hall effect transmitting compass according to any preceding claim, wherein the Hall effect sensors are connected to a circuit for evaluation values sensed by the sensors and for giving an indication of the associated compass heading.
6. A Hall effect transmitting compass substantially as described herein with reference to the drawings.
GB08333814A 1983-12-20 1983-12-20 Hall effect transmitting compass Withdrawn GB2151790A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08333814A GB2151790A (en) 1983-12-20 1983-12-20 Hall effect transmitting compass

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08333814A GB2151790A (en) 1983-12-20 1983-12-20 Hall effect transmitting compass

Publications (1)

Publication Number Publication Date
GB2151790A true GB2151790A (en) 1985-07-24

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Family Applications (1)

Application Number Title Priority Date Filing Date
GB08333814A Withdrawn GB2151790A (en) 1983-12-20 1983-12-20 Hall effect transmitting compass

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GB (1) GB2151790A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2167191A (en) * 1984-11-16 1986-05-21 David Louis Halsey Person Hall-effect attitude sensors
US4599564A (en) * 1983-11-07 1986-07-08 Rca Corporation Tubular semiconductor magnetic field sensor and circuits for use therewith
EP0713162A1 (en) * 1994-11-21 1996-05-22 Asulab S.A. Watch with device for determining the direction of earth magnetic north
EP0721155A1 (en) * 1995-01-04 1996-07-10 Asulab S.A. Watch comprising a device indicating a predetermined geographical location
CH688731A5 (en) * 1994-06-21 1998-02-13 Keller Gmbh A process for the manufacture of a hollow chocolate body, and hollow chocolate bodies.
US5721713A (en) * 1995-01-04 1998-02-24 Asulab S.A. Watch comprising an arrangement for indicating a predetermined geographic locality

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1543895A (en) * 1976-02-19 1979-04-11 Thomsen I Detector for detecting the angular position of a rotatable magnet

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1543895A (en) * 1976-02-19 1979-04-11 Thomsen I Detector for detecting the angular position of a rotatable magnet

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4599564A (en) * 1983-11-07 1986-07-08 Rca Corporation Tubular semiconductor magnetic field sensor and circuits for use therewith
GB2167191A (en) * 1984-11-16 1986-05-21 David Louis Halsey Person Hall-effect attitude sensors
CH688731A5 (en) * 1994-06-21 1998-02-13 Keller Gmbh A process for the manufacture of a hollow chocolate body, and hollow chocolate bodies.
EP0713162A1 (en) * 1994-11-21 1996-05-22 Asulab S.A. Watch with device for determining the direction of earth magnetic north
CH687288GA3 (en) * 1994-11-21 1996-11-15 Asulab Sa Watch including a device for detecting the direction of terrestrial magnetic north.
US5596551A (en) * 1994-11-21 1997-01-21 Asulab S.A. Watch comprising an arrangement for detecting the direction of the terrestrial magnetic north
EP0721155A1 (en) * 1995-01-04 1996-07-10 Asulab S.A. Watch comprising a device indicating a predetermined geographical location
US5721713A (en) * 1995-01-04 1998-02-24 Asulab S.A. Watch comprising an arrangement for indicating a predetermined geographic locality
CH688949GA3 (en) * 1995-01-04 1998-06-30 Asulab Sa Watch comprising a display device of a predetermined geographical location.

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WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)