INTEGRATED TILT COMPENSATED COMPASS IN A SINGLE PACKAGE

• US 20090093981A1
• Filed: 10/05/2007
• Published: 04/09/2009
• Est. Priority Date: 10/05/2007
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Withanawasam, Lakshman
• Application Number:
  US11/868,390
• Publication Number:
  US 20090093981A1
• Time in Patent Office: Days
• US Class Current: 702/93
• CPC Class Codes: G01C 17/28 Electromagnetic compasses with north seeking magnetic elements and having electric pick-offs G01C17/26
• CPC Class Codes: G01C 17/38 Testing, calibrating, or compensating of compasses

Abstract

A magnetic compass includes a magnetic sensor, an acceleration sensor, respective signal conditioning circuits in electronic communication with the sensors and a microprocessor. These components are arranged and structurally coupled to a single electronic package that supports the sensors, the signal conditioning circuits, and the microprocessor to provide a miniaturized magnetic compass. In addition, a temperature sensor may be coupled to the package to provide temperature compensation for at least some of the above-identified components.

Claims

1. A magnetic compass comprising:

a magnetic sensor;

a first signal conditioning circuit in signal communication with the magnetic sensor;

an acceleration sensor;

a second signal conditioning circuit in signal communication with the acceleration sensor;

a microprocessor in signal communication with the first and second signal conditioning circuits; and

a single electronic package configured to structurally support and to electrically interconnect, the sensors, the signal conditioning circuits, and the microprocessor in an integrated arrangement, wherein the sensors, the signal conditioning circuits, and the microprocessor interact to provide signal conditioning and compass computations.

2. The magnetic compass of claim 1 wherein the acceleration sensor includes at least two magnetic field sensing axes arranged for detecting magnetic field components.

3. The magnetic compass of claim 1 wherein the acceleration sensor includes three magnetic field sensing axes arranged substantially orthogonal to one another for detecting magnetic field components.

4. The magnetic compass of claim 1 wherein the acceleration sensor includes at least two acceleration sensing axes arranged to detect an acceleration.

5. The magnetic compass of claim 1 wherein the acceleration sensor includes three acceleration sensing axes arranged substantially orthogonal to one another for detecting an acceleration.

6. The magnetic compass of claim 1 wherein the second signal conditioning circuits are integrated.

7. The magnetic compass of claim 1, further comprising a temperature sensor attached to the package in signal communication with the microprocessor.

8. The magnetic compass of claim 1, wherein the temperature sensor is configured to provide temperature compensation to at least one of the sensed signals.

9. The magnetic compass of claim 1, wherein the single electronic package is made from the group consisting of plastic, silicon, and a laminate.

10. The magnetic compass of claim 1, wherein the first signal processing circuit is configured as an application-specific integrated circuit for processing signals from the magnetic sensor.

11. The magnetic compass of claim 1, wherein the second signal processing circuit is configured as an application-specific integrated circuit for processing signals from the acceleration sensor.

12. The magnetic compass of claim 1, wherein the single electronic package is constructed to enable integrating the magnetic compass, via surface mount technology, onto a next level assembly.

13. The magnetic compass of claim 1, wherein the single electronic package can be assembled vertically or horizontally, and in any orientation.

14. The magnetic compass of claim 1, wherein the microprocessor is operable to take a compass heading when the single electronic package is arranged in a desired orientation.

15. A method of arranging electrical components of a magnetic compass to produce compass-related computations, the method comprising:

structurally attaching a magnetic sensor, an acceleration sensor, and signal conditioning circuits onto a single electronic package;

centrally locating and structurally attaching a microprocessor on the package such that the microprocessor is in electrical communication with at least the signal conditioning circuits;

detecting a tilt angle of the compass with the acceleration sensor and providing a signal representative of the tilt angle to the microprocessor;

detecting a magnetic field with the magnetic sensor and providing a signal representative of the magnetic heading to the microprocessor; and

outputting a tilt angle and magnetic heading based on a detected tilt angle and magnetic heading of the compass.

16. The method of claim 15, wherein structurally attaching the magnetic sensor, the acceleration sensor, and the signal conditioning circuits onto the single electronic package includes using surface mount technology.

17. The method of claim 15, wherein outputting includes interfacing with a serial device via a data communication port.

18. The method of claim 15, wherein outputting includes performing temperature compensation based on a sensed temperature of the package.

19. The method of claim 15, further comprising sensing a temperature of the package with a temperature sensor located and coupled to the package.

20. The method of claim 15, further comprising sensing compensating sensor biases arising from attaching the magnetic compass onto a next level assembly.