Automatic heading and reference system

• US 20070088496A1
• Filed: 07/20/2005
• Published: 04/19/2007
• Est. Priority Date: 07/20/2005
• Status: Abandoned Application

• Current Assignee: Atair Aerospace, Inc.
• Original Assignee: Atair Aerospace, Inc.
• Inventors: Preston, Daniel
• Application Number:
  US11/185,410
• Publication Number:
  US 20070088496A1
• Time in Patent Office: Days
• US Class Current: 701/207
• CPC Class Codes: G01C 17/30 Earth-inductor compasses
• CPC Class Codes: G01C 17/38 Testing, calibrating, or compensating of compasses
• CPC Class Codes: G01C 21/005 with correlation of navigation data from several sources, e.g. map or contour matching G01C21/30 takes precedence

Abstract

A sensor system and method is disclosed which is substantially non-shock sensitive, inexpensive and small enough to be incorporated into most applications. The sensor system includes a magnetometer (preferably a triaxial magnetometer) and at least one infrared sensor. In the preferred embodiment, the sensor system includes at least four infrared sensors arranged substantially orthogonal to each other in a common plane horizontal to the earth'"'"'s surface. The infrared sensors generate signals that are analyzed by a processor to determine the tilt orientation of the object. Based on the tilt orientation of the object, the magnetometer is tilt compensated (preferably fully compensated). The sensor system may also include a global positioning system.

Claims

1. A method of tilt compensating a magnetometer comprising the acts of:

receiving a first signal from an infrared sensor;

receiving at least a second signal from said infrared sensor;

calculating a difference between said first and said at least a second signal;

determining a tilt of said magnetometer based on said difference between said first and said at least a second signal; and

tilt compensating said magnetometer based on said tilt of said magnetometer.

2. The method as claimed in claim 1 wherein said method includes:

receiving a first signal from a first infrared sensor; and

receiving at least a second signal from at least a second infrared sensor.

3. The method as claimed in claim 2 further including at least four infrared sensors directed substantially 90 degrees apart in substantially parallel plane to each other.

4. The method as claimed in claim 3 wherein said at least two infrared sensors are directed substantially towards the ground and at least two infrared sensors are directed towards the sky.

5. The method as claimed in claim 1 wherein said first and said at least a second signal are generated by a single infrared sensor.

6. The method as claimed in claim 1 wherein said magnetometer includes at least three magnetometers arranged substantially orthogonal to each other.

7. The method as claimed in claim 1 wherein said magnetometer includes a triaxial magnetometer.

8. The method as claimed in claim 1 wherein said magnetometer includes at least three magnetometers arranged substantially orthogonal to each other.

9. A system for determining an orientation of an object comprising:

at least one magnetometer secured to said object;

at least one infrared sensor secured to said object; and

a processor, said processor comparing an output signal generated by said at least one infrared sensor to determine a tilt of said sensor, wherein said processor tilt compensates said at least one magnetometer in response to said tilt of said object.

10. The system as claimed in claim 9 wherein said at least one magnetometer includes at least three magnetometers arranged substantially orthogonal to each other.

11. The method as claimed in claim 9 wherein said at least one magnetometer includes at least one triaxial magnetometer.

12. The system as claimed in claim 9 wherein said at least one infrared sensor includes at least four infrared sensors directed substantially 90 degrees apart in substantially parallel planes to each other.

13. The system as claimed in claim 12 wherein at least two of said infrared sensors are directed substantially towards the earth and at least two of said infrared sensors are directed towards the sky.

14. The system as claimed in claim 12 wherein further including eight infrared sensors wherein two infrared sensors are directed in each of the four directions, and wherein each of said four directions includes a first infrared sensor directed substantially towards the earth at approximately a 45 degree angle from the horizon and wherein a second infrared sensors is directed substantially towards the sky at approximately a 45 degree angle from the horizon.

15. The system as claimed in claim 9 further including at least one of the following sensors selected from the group consisting of accelerometers and gyroscopes.

16. The system as claimed in claim 15 wherein said processor further includes switching software, wherein said switching software determines at least one of the available sensors which is most appropriate given the operating conditions and selects said at least one appropriate sensor.

17. The system as claimed in claim 9 further including a global positioning system coupled to said processor.

18. A system for determining an orientation of an object comprising:

at least four infrared sensors secured to said object, said at least four infrared sensors directed substantially 90 degrees apart in substantially parallel planes to each other;

a triaxial magnetometer secured to said object; and

a processor coupled to said at least four infrared sensors and said triaxial magnetometer, said processor receiving output signals from said at least four infrared sensors and calculating a tilt of said object based on a difference between said signals and compensating said magnetometer based on said calculated tilt.

19. The system as claimed in claim 18 further including a global positioning system coupled to said processor.

20. The system as claimed in claim 18 further including at least one of the following sensors selected from the group consisting of accelerometers and gyroscopes, wherein said processor further includes switching software for determining at least one of the available sensors which is most appropriate given the operating conditions and for selecting said at least one appropriate sensor.