Magnetic compass

• US 5,095,631 A
• Filed: 11/06/1990
• Issued: 03/17/1992
• Est. Priority Date: 11/07/1989
• Status: Expired due to Fees

• Current Assignee: The State of Israel Ministry of Defense Armament Development Authority
• Original Assignee: The State of Israel Ministry of Defense Armament Development Authority
• Inventors: Netzer, Yshay, Mor, Avigdor, Gavril, Solomon, Zeiler, Eitan
• Primary Examiner(s): Cuchlinski, Jr., William A.
• Assistant Examiner(s): FULTON, CHRISTOPHER W
• Application Number:
  US07/609,617
• Time in Patent Office: 497 Days
• Field of Search: 33/361, 33/356, 33/357, 33/362, 33/333, 33/340, 33/365, 33/370, 73/1 E
• US Class Current: 33/361
• CPC Class Codes: G01C 17/38 Testing, calibrating, or compensating of compasses

Abstract

An electronic compass system for determining the heading of an armored vehicle containing a large mass of ferromagnetic material, which system comprises a plurality of sensors, and for real-time computation of the corrections required of actual magnetometer measurements. Part of the values used for the computation are computed in advance, and part in real-time. Some of the computations are based on the perturbation of the earth magnetic field based on an algorithm which takes into account one or two rotational prolate ferromagnetic ellipsoids which have certain dimensions and which are at a predetermined distance from each other either represent the body of an armored vehicle, or when two ellipsoids are used, they represent the hull and turret of a tank.

Claims

1. An electronic magnetic compass system for determining the heading of a portion of a heavily armored vehicle, comprising in combination:

a biaxial fluxgate magnetometer positioned in an antenna-like structure in a position above a highest level of the vehicle for determining magnetic field components with respect to the vehicle;

two inclinometers for determining pitch and tilt angles of the vehicle with respect to a horizontal plane;

computing means for geometric correction of the magnetic field components dependent on the pitch and tilt angles, for determining iron body perturbation of the local magnetic field of the earth due to one or more rotational prolate ferromagnetic ellipsoids of predetermined dimensions and position relative to each other, representing iron body portions of said vehicle, for perturbation correction of the magnetic field components, and for determining the heading of a portion of the vehicle dependent on the geometric and perturbation corrections.

2. A system according to claim 1, further comprising external computer means attached to a magnetic compass for determining a position for installing the magnetometer for a specific class of armored vehicles and for each individual member of such class.

3. A system according to claim 1, in which

the magnetometer and inclinometers continually generate measurement signals in real time and

computing means continually determines corrected heading in real time and include:

means for determining the components of the magnetic field in the horizontal plane dependent on pitch and tilt angles and on magnetic field components measured along the axes of the fluxgate magnetometer,

means for determining iron-body perturbation values,

means for subtracting the perturbation values from the magnetic field components in the horizontal plane,

means for determining the corrected azimuth and

means for displaying the results which indicate the heading of the vehicle.

4. A system according to claim 1, in which computing means include means for determining the iron body perturbation of the local magnetic field of the earth depending on a limited number of parameters depending on the class of the vehicle.

5. A system according to claim 1, in which computing means include means for:

projecting measured components of the magnetic field to the horizontal plane;

determining an approximate heading of the vehicle;

determining iron body perturbation;

correcting projected magnetic field components dependent on said perturbation;

determining a corrected azimuth based on the corrected components;

checking results for convergence based on the corrected azimuth to determine accuracy of results; and

continuing such correcting of components, determining of azimuth and checking of convergence depending upon the accuracy of results.

6. A system according to claim 1, further comprising external computing means for:

determining optimum magnetometer location depending on calibration files gathered during a setup stage of said compass system; and

determining dimensions and relative position of said ellipsoids upon which said determination of iron body perturbation depends.

7. A system according to claim 6, in which, in order to optimize correction of the magnetic field components, said external computing means include means for:

inputting, during a data acquisition stage in which a true magnetic heading is known, magnetic field inclination angle signals for a set of traverse angles of the portions of the vehicle with respect to each other;

determining optimum values for fixed magnetization of said ellipsoids;

determining optimum dimensions and position of said ellipsoids;

determining optimum magnetic permeability for said ellipsoids;

determining optimum positioning for the magnetometer; and

outputting result signals for said determinations.

9. A system according to claim 1, in which computing means include, means for computing the values of δ

H_x and δ

H_y by an iterative process and for subtracting these from the measured values H_x and H_y of the magnetometer for providing a corrected azimuth angle.

10. A system of claim 1, in which:

the armored vehicle is a main battle tank including a hull and a rotatable turret bearing a gun;

the perturbation due to two independently rotatable ferromagnetic ellipsoids representing the hull and turret of the tank is determined; and

the system further comprises;

means for measuring the angle between the hull and the turret.

12. The system of claim 1, in which computing means include apparatus representing the following equations for converting input signals H_x and H_y corresponding to measured magnetic field components in the horizontal plane into output signals δ

H_x and δ

H_y, corresponding to unperturbed magnetic field components;

##EQU4##

8. A system for measurement with adequate accuracy the heading of a heavily armored vehicle by compass means, by correcting magnetic perturbations due to residual and temporary magnetization of the body of such vehicle, which system comprises:

a biaxial fluxgate magnetometer on the vehicle in a position selected to optimize correction of flux measurement signals generated by the magnetometer;

pendulum-type inclinometers for outputting electrical measurement signals corresponding to inclination angles of the vehicle with respect to horizontal plane;

an A/D+MUX card for receiving and processing such measurement signals;

a microprocessor based unit communicating with such card for real time signal corrections;

a non-volatile memory apparatus communicating with the microprocessor to direct microprocessor function based on models within the memory representing mathematical procedures;

control and display panels in the vehicle for displaying signals output from the microprocessor;

interconnecting cables between the above parts,

and in which the memory includes a model of one or more prolate ferromagnetic ellipsoids of predetermined size and position relative to each other representing respective portions of the vehicle to direct the microprocessor to correct signals input from the card to generate corrected signals output to the panels.

11. The system of claim 8, in which:

the heavily armored vehicle is a main battle tank with a hull and a turret bearing a gun;

the memory includes a model of two ellipsoids representing the turret and hull respectively; and

the system further comprises;

an angle measuring device for determining the angle of rotation between the turret and hull.