Measurement of magnetic field gradients

Patent metadata

Field	Value
Publication number	US-10338261-B2
Application number	US-201514856356-A
Country	US
Kind code	B2
Filing date	Sep 16, 2015
Priority date	Sep 16, 2015
Publication date	Jul 2, 2019
Grant date	Jul 2, 2019

Abstract

Technology for performing magnetic field gradient measurements is described. The magnetic field gradient measurements for specific positions on the Earth can be performed from a moving platform. The magnetic field gradient measurements can be identified as being affected by a level of error that exceeds a defined threshold. A correction value can be generated to compensate for the error in the magnetic field gradient measurements. The correction value can be applied to the magnetic field gradient measurements in order to obtain magnetic field gradient measurements with a reduced level of error.

First claim

What is claimed is:

1. A system for performing magnetic field gradient measurements, the system comprising:
an inductive coil vector magnetometer that is onboard a moving platform, the inductive coil vector magnetometer operable to perform the magnetic field gradient measurements for specific positions on the Earth from the moving platform;
a gyroscope, coupled to the vector magnetometer, that is operable to generate a correction value to compensate for error in the magnetic field gradient measurements captured by the inductive coil vector magnetometer; and
one or more processors operable to:
identify that the magnetic field gradient measurements are affected by a level of error that exceeds a defined threshold;
identify the correction value generated at the gyroscope to compensate for the error in the magnetic field gradient measurements; and
apply the correction value generated at the gyroscope to the magnetic field gradient measurements in order to obtain magnetic field gradient measurements with a reduced level of error,
wherein the correction value received from the gyroscope comprises a relative rotation matrix and is applied to the magnetic field gradient measurements to relate a coil vector magnetometer antenna and an airframe body coordinate system to compensate for high frequency airframe vibrations that causes disorientation of the inductive coil vector magnetometer.

2. The system of claim 1 , wherein the correction value compensates for a misalignment between an orientation of the airframe body coordinate system associated with the moving platform and an orientation of the magnetometer onboard the moving platform.

3. The system of claim 1 , wherein the error is caused by the high frequency airframe vibrations on the moving platform due to a speed of the moving platform.

4. The system of claim 1 , wherein the magnetic field gradient measurements are performed according to a range of approximately 2000 to 50,000 times per second.

5. The system of claim 1 , wherein a magnetic field gradient measurement is a projection of a magnetic field gradient tensor into a direction of motion associated with the moving platform.

6. The system of claim 1 , wherein the moving platform is traveling at a defined velocity of Mach 0.5 or greater.

7. The system of claim 1 , wherein the moving platform is a self-propelled guided weapon or an aircraft.

8. A system for determining a magnetic field gradient, the system comprising:
a vector magnetometer onboard a moving platform;
a gyroscope onboard the moving platform and coupled to the vector magnetometer; and
one or more processors operable to:
measure the magnetic field gradient for specific positions on the Earth using the vector magnetometer onboard the moving platform, the magnetic field gradient being affected by error that is caused by an orientation misalignment of the vector magnetometer and a body coordinate system of the moving platform;
generate a correction value to compensate for the error in the magnetic field gradient using the gyroscope that is onboard the moving platform; and
apply the correction value to the magnetic field gradient in order to reduce the error in the magnetic field gradient caused by the orientation misalignment of the vector magnetometer,
wherein the correction value comprises a relative rotation matrix and is applied to the magnetic field gradient to relate a coil vector magnetometer antenna and an airframe body coordinate system to compensate for high frequency airframe vibrations that causes disorientation of the inductive coil vector magnetometer.

9. The system of claim 8 , wherein the one or more processors are further operable to generate the correction value to compensate for the error in the magnetic field gradient when an error level exceeds a defined threshold.

10. The system of claim 8 , wherein the one or more processors are further operable to generate the correction value to compensate for the error in the magnetic field gradient when the moving platform is traveling at a velocity that exceeds a defined threshold.

11. The system of claim 8 , wherein the one or more processors are further operable to generate the correction value to compensate for the error in the magnetic field gradient when the moving platform is traveling at a defined velocity of Mach 0.5 or greater.

12. The system of claim 8 , wherein the correction value is provided by the gyroscope onboard the moving platform.

13. The system of claim 8 , wherein the error is caused by the high frequency airframe vibrations on the moving platform due to a speed of the moving platform.

14. The system of claim 8 , wherein the magnetic field gradient is of the Earth's magnetic anomaly field.

15. The system of claim 8 , wherein the one or more processors are further operable to determine the magnetic field gradient by converting the magnetic field gradient from a local coordinate system to a North East Down (NED) coordinate system of the moving platform.

16. A system for determining a magnetic field gradient, the system comprising:
a vector magnetometer operable to measure the magnetic field gradient for specific positions on the Earth;
a gyroscope, coupled to the vector magnetometer, that is operable to generate a correction value to compensate for error in the magnetic field gradient; and
one or more processors operable to:
identify the magnetic field gradient;
identify the correction value; and
apply the correction value to the magnetic field gradient,

wherein the vector magnetometer and the gyroscope are onboard a moving platform,
wherein the correction value received from the gyroscope comprises a relative rotation matrix and is applied to the magnetic field gradient to relate a coil vector magnetometer antenna and an airframe body coordinate system to compensate for high frequency airframe vibrations that causes disorientation of the inductive coil vector magnetometer.

17. The system of claim 16 , wherein the gyroscope is operable to generate the correction value when the error in the magnetic field gradient exceeds a defined threshold and the moving platform is traveling at a defined velocity.

18. The system of claim 16 , wherein the error in the magnetic field gradient is caused by a misalignment of a local coordinate system associated with the moving platform and an orientation of the vector magnetometer.

Assignees

• Raytheon Co

Inventors

• Gann Matthew E
• Dolgin Benjamin
• Zellner James C
• Barillas Ender E

Classifications

• G01D18/004

  Continuous recalibration · CPC title

• G01C21/08

  involving use of the magnetic field of the earth · CPC title

• G01R33/022

  Measuring gradient · CPC title

• G01V3/165

  operating with magnetic or electric fields produced or modified by the object or by the detecting device (with electromagnetic waves G01V3/17) · CPC title

• G01C25/005

  initial alignment, calibration or starting-up of inertial devices · CPC title