Electronic magnetic compass system

• US 4,686,772 A
• Filed: 05/27/1986
• Issued: 08/18/1987
• Est. Priority Date: 05/23/1986
• Status: Expired due to Fees

• Current Assignee: Elbit Computers, Ltd.
• Original Assignee: Elbit Computers, Ltd.
• Inventors: Sobel, Amos
• Primary Examiner(s): Stearns, Richard R.
• Application Number:
  US06/866,719
• Time in Patent Office: 448 Days
• Field of Search: 33/333, 33/352, 33/356, 33/361, 73/1 E
• US Class Current: 33/333
• CPC Class Codes: G01C 17/38 Testing, calibrating, or compensating of compasses

Abstract

An electronic magnetic compass for computing the magnetic heading of a vehicle, such as a tank, having two iron bodies relatively movable with respect to each other about a vertical rotary axis comprises: a non-pendulous triaxial magnetometer outputting magnetic field electrical signals representing the three axial components of the magnetic field at the location of the magnetometer; sensors outputting electrical signals representing the pitch and roll of the vehicle body on which the sensors are mounted; an angle measuring device for outputting electrical signals corresponding to the angle of rotation between the two bodies; a memory for storing a plurality of pre-calibrated correction factors for correcting the effects of the permanent magnetic field and the induced magnetic field on the measurements of the magnetometer for each of a plurality of angles of rotation between the two bodies; and an electronic computer for computing on a real-time basis the magnetic heading of both bodies from the magnetic field electrical signals as corrected by the stored correction factors for the respective angle of rotation, together with the pitch, roll and rotation angles electrical signals inputted into the computer.

Claims

1. An electronic magnetic compass system for computing the magnetic heading of a vehicle having two iron bodies relatively movable with respect to each other about a vertical rotary axis comprising;

a non-pendulous triaxial magnetometer to be fixedly mounted on one of said bodies for outputting electrical signals corresponding to the three axial components on the magnetic field at the location of the magnetometer;

a first sensor on said one body for outputting electrical signals corresponding to the pitch of said one body;

a second sensor on said one body for outputting electrical signals corresponding to the roll of said one body;

an angle measuring device for outputting electrical signals corresponding to the angle of rotation between said two bodies about said vertical rotary axis;

a non-volatile memory for storing a plurality of pre-calibrated correction factors for correcting the effects of the permanent magnetic field and the induced magnetic field on the measurements of the magnetometer for each of a plurality of angles of rotation between the two bodies;

and an electronic computer for computing on a real-time basis the magnetic headings of both said bodies from said magnetic field electrical signals, as corrected by said stored correction factors for the respective angle of rotation, together with the pitch, roll and rotation angles electrical signals inputted into the computer.

2. The system according to claim 1, wherein the vehicle is a tank having a turret rotatably mounted on a hull, said magnetometer, pitch sensor and roll sensor being mounted on said turret.

3. The system according to claim 2, wherein said electronic computer makes the following computations on a real time basis:

space="preserve" listing-type="equation">A=T.sub.θ

.sup.-1 T.sub.φ

.sup.-1 W(α

)[M-H(α

)]

space="preserve" listing-type="equation">B=T.sub.α

.sup.-1 A

space="preserve" listing-type="equation">Ψ

.sub.T =δ

-tg.sup.-1 Ay/Ax

space="preserve" listing-type="equation">Ψ

.sub.H =δ

-tg.sup.-1 By/Bx

wherein;

A, B,--intermediate calculation vectors;

Ψ

_T --turret magnetic heading corrected by local declination;

Ψ

_H --hull magnetic heading corrected by local declination;

δ

--local declination;

M--magnetometer readings vector;

H(α

)--permanent magnetism correction vector as a function of traverse angle;

W(α

)--induced magnetism correction matrix as a function of traverse angle;

φ

--turret roll;

T.sub.φ

^-1 --Euler inverse rotation matrix in roll;

θ

--turret pitch;

T.sub.θ

^-1--Euler inverse rotation matrix in pitch.

α

--traverse angle; and

T.sub.α

^-1 --Euler inverse rotation matrix in traverse angle.

4. The system according to claim 1, wherein said pitch sensor and roll sensor are two non-parallel inclinometers.

5. The system according to claim 1, wherein said electronic computer includes a real-time computer for computing magnetic headings on a real-time basis, and a calibration computer for computing the calibration correction factors which are stored in said non-volatile memory of the real-time computer.

6. The system according to claim 5, wherein said calibration computer is a separate unit distinct from and detachable from the real-time computer after the calibration has been completed.

7. The system of claim 5, wherein said calibration computer performs the following operations:

during a data acquisition stage where the true or magnetic heading is known, inputs the magnetic field, pitch and roll values for each of a plurality of traverse angles of one of said iron bodies with respect to the other of said iron bodies;

for each of a plurality of traverse angles, calculates an induced magnetism correction matrix and a permanent magnetism correction vector;

and stores said correction matrix and correction vector for each of the said plurality of traverse angles in said non-volatile memory of the real-time computer.

8. The system according to claim 7, wherein said system is calibrated by said computer for 16 evenly-spaced traverse angles.

9. An electronic magnetic compass system for computing the magnetic heading of a tank having a turret rotatable on a hull about a vertical rotary axis comprising;

a non-pendulous triaxial magnetometer to be fixed mounted on said turret for outputting electrical signals corresponding to the three axial components on the magnetic field at the location of the magnetometer;

a first sensor on said turret for outputting electrical signals corresponding to the pitch of said turret;

a second sensor on said turret for outputting electrical signals corresponding to the roll of said turret;

an angle measuring device for outputting electrical signals corresponding to the angle of rotation between said turret and about said vertical rotary axis;

a non-volatile memory for storing a plurality of pre-calibrated correction factors for correcting the effects of the permanent magnetic field and the induced magnetic field on the measurements of the magnetometer for each of a plurality of angles of rotation between the turret with respect to the hull;

and an electronic computer for computing on a real-time basis the magnetic headings of both said turret and hull from said magnetic field electrical signals, as corrected by said stored correction factors for the respective angle of rotation, together with the pitch, roll and rotation angles electrical signals inputted into the computer.

10. The system according to claim 9, wherein said pitch, sensor and roll sensor are two non-parallel inclinometers.

11. The system according to claim 9, wherein said electronic computer includes a real-time computer for computing magnetic headings on a real-time basis, and a calibration computer for computing the calibration correction factors which are stored in said non-volatile memory of the real-time computer.

12. The system according to claim 11, wherein said calibration computer is a separate unit distinct from and detachable from the real-time computer after the calibration has been completed.

13. The system of claim 11, wherein said calibration computer performs the following operations:

during a data acquisition stage where the true or magnetic heading is known, inputs the magnetic field, pitch and roll values for each of a plurality of traverse angles of the turret with respect to the hull;

for each of a plurality of traverse angles, calculates an induced magnetism correction matrix and a permanent magnetism correction vector;

and stores said correction matrix and correction vector for each of the said plurality of traverse angles in said non-volatile memory of the real-time computer.

14. The system according to claim 13, wherein said system is calibrated by said computer for 16 evenly-spaced traverse angles.