Inertial measurement system with self correction

• US 8,010,308 B1
• Filed: 11/24/2008
• Issued: 08/30/2011
• Est. Priority Date: 11/23/2007
• Status: Active Grant

• Current Assignee: Hottinger Bruel & Kjaer Incorporated
• Original Assignee: MicroStrain, Inc. (Spectris PLC)
• Inventors: Churchill, David L.
• Primary Examiner(s): Cosimano; Edward R
• Application Number:
  US12/277,244
• Time in Patent Office: 1,009 Days
• Field of Search: 73/10.1, 73/13.7, 73/13.8, 73/17.5, 73/17.6, 73/17.7, 73/17.9, 73/18.1, 731/78.R, 734/321, 738/658, 738/659, 701/1, 701/200, 701/224, 702/1, 702/85, 702/92, 702/93, 702/104, 702/127, 702/150, 702/151, 702/154, 702/187, 702/189
• US Class Current: 702/104
• CPC Class Codes: G01C 21/188 for accumulated errors, e.g. by coupling inertial systems with absolute positioning systems
• CPC Class Codes: G01C 25/005 initial alignment, calibration or starting-up of inertial devices

Abstract

A method of navigation includes providing an angular rate sensor and a direction-of-gravity reference. The method also includes determining bias error of the angular rate sensor about a vertical axis based on data substantially from the angular rate sensor and from the direction-of-gravity reference. In one embodiment, the first angular rate sensor is moved from a first position around a substantially horizontal axis to a second position around the substantially horizontal axis. The first angular rate sensor provides angular rate data for attitude at the first position and for compass heading at the second position. Data from the first angular rate sensor and from the direction-of-gravity reference is processed with a program for determining a bias error correction for the first angular rate sensor while the first angular rate sensor is in the first position. Bias error correction determined while the first angular rate sensor is in the first position is used to correct angular rate of the first angular rate sensor while the first angular rate sensor is in the second position.

Claims

1. A method, comprising:

a. providing an angular rate sensor and a direction-of-gravity reference; and

b. determining bias error of said angular rate sensor about a vertical axis based on data substantially from said angular rate sensor and from said direction-of-gravity reference.

2. A method as recited in claim 1, wherein said determining bias error of said angular rate sensor about a vertical axis is based on data exclusively from said angular rate sensor and from said direction-of-gravity reference.

3. A method as recited in claim 1, wherein said direction-of-gravity reference includes at least one accelerometer.

4. A method as recited in claim 1, further comprising tumbling said angular rate sensor around a substantially horizontal axis.

5. A method as recited in claim 1, wherein said providing an angular rate sensor and a direction-of-gravity reference involves providing triaxial angular rate sensors and triaxial accelerometers, wherein said triaxial angular rate sensors are approximately orthogonally mounted, and wherein said triaxial accelerometers are approximately orthogonally mounted, and wherein said triaxial angular rate sensors and said triaxial accelerometers are mounted in a housing, wherein said housing includes an motor for tumbling said triaxial angular rate sensors around said substantially horizontal axis.

6. A method as recited in claim 1, wherein said angular rate sensor primarily provides angular rate data for attitude for a first fraction of time and wherein said angular rate sensor primarily provides angular rate data for compass heading for a second fraction time, wherein said first fraction and said second fraction are substantially equal.

7. A method as recited in claim 1, further comprising mounting said angular rate sensor and said direction-of-gravity reference on a structure.

8. A method as recited in claim 7, wherein said structure includes an article for wearing by a person.

9. A method as recited in claim 8, wherein said article for wearing by a person includes footwear.

10. A method as recited in claim 1, further comprising moving said angular rate sensor from a first position around a substantially horizontal axis to a second position around said substantially horizontal axis, wherein said angular rate sensor provides angular rate data for attitude at said first position and for compass heading at said second position.

11. A method as recited in claim 10, wherein said moving said angular rate sensor involves using a motor to move said angular rate sensor.

12. A method as recited in claim 11, wherein said angular rate sensor has a bias time constant, wherein said motor provides tumbling, wherein period of tumbling is less than said bias time constant.

13. A method as recited in claim 10, further comprising processing data from said angular rate sensor and from said direction-of-gravity reference with a program for determining a bias error correction for said angular rate sensor while said angular rate sensor is in said first position.

14. A method as recited in claim 13, further comprising using said bias error correction determined while said angular rate sensor is in said first position to correct angular rate of said angular rate sensor while said angular rate sensor is in said second position.

15. A method as recited in claim 13, wherein said processing data involves using a processor.

16. A method as recited in claim 15, further comprising providing said processor to move with said angular rate sensor.

17. A method as recited in claim 16, further comprising providing a transceiver to move with said angular rate sensor, and using said transceiver to transmit corrected heading data.

18. A method as recited in claim 17, further comprising using said transceiver to transmit corrected velocity and position data.

19. A method, comprising

a. providing an angular rate sensor and an inertial sensor;

and

b. determining bias error of said angular rate sensor about a vertical axis based on data substantially from said angular rate sensor and from said inertial sensor.

20. A method as recited in claim 19, wherein said determining bias error of said angular rate sensor about a vertical axis is based on data exclusively from said angular rate sensor and from said inertial sensor.

21. A method as recited in claim 19, wherein said angular rate sensor primarily provides angular rate data for attitude for a first fraction of time and wherein said angular rate sensor primarily provides angular rate data for compass heading for a second fraction time, wherein said first fraction and said second fraction are substantially equal.

22. A method of navigation, comprising

a. providing an angular rate sensor and a direction-of-gravity reference;

b. moving said angular rate sensor from a first position around a substantially horizontal axis to a second position around said substantially horizontal axis, wherein said angular rate sensor provides angular rate data for attitude at said first position and for compass heading at said second position;

c. processing data from said angular rate sensor and from said direction-of-gravity reference with a program for determining a bias error correction for said angular rate sensor while said angular rate sensor is in said first position; and

d. using said bias error correction determined while said angular rate sensor is in said first position to correct angular rate of said angular rate sensor while said angular rate sensor is in said second position.

23. A method as recited in claim 22, wherein said direction-of-gravity reference includes at least one accelerometer.

24. A method as recited in claim 22, wherein said providing an angular rate sensor and a direction-of-gravity reference involves providing triaxial angular rate sensors and triaxial accelerometers, wherein said triaxial angular rate sensors are approximately orthogonally mounted, and wherein said triaxial accelerometers are approximately orthogonally mounted, and wherein said triaxial angular rate sensors and said triaxial accelerometers are mounted in a housing, wherein said housing includes a motor for tumbling said triaxial angular rate sensors around said substantially horizontal axis.

25. A method as recited in claim 22, wherein said angular rate sensor primarily provides angular rate data for attitude for a first fraction of time and wherein said angular rate sensor primarily provides angular rate data for compass heading for a second fraction time, wherein said first fraction and said second fraction are substantially equal.

26. A method as recited in claim 22, wherein said moving said angular rate sensor involves using a motor to move said angular rate sensor.

27. A method as recited in claim 26, wherein said angular rate sensor has a bias time constant, wherein said motor provides tumbling, wherein period of tumbling is less than said bias time constant.

28. A method as recited in claim 22, further comprising mounting said angular rate sensor and said direction-of-gravity reference on a structure.

29. A method as recited in claim 28, wherein said moving said angular rate sensor involves moving said structure.

30. A method as recited in claim 29, wherein said structure includes an article for wearing by a person.

31. A method as recited in claim 30, wherein said article for wearing by a person includes footwear.

32. A method as recited in claim 22, wherein said processing data involves using a processor.

33. A method as recited in claim 32, further comprising providing said processor to move with said angular rate sensor.

34. A method as recited in claim 33, further comprising providing a transceiver to move with said angular rate sensor, and using said transceiver to transmit corrected heading data.

35. A method as recited in claim 34, further comprising using said transceiver to transmit corrected velocity and position data.

36. A sensing unit, comprising:

a direction-of-gravity reference and an angular rate sensor;

an actuator mounted to provide movement of said angular rate sensor from a first position around a substantially horizontal axis to a second position around said substantially horizontal axis, wherein said angular rate sensor provides angular rate data for attitude at said first position and wherein said angular rate sensor provides angular rate data for compass heading at said second position; and

a processor connected to receive data from said angular rate sensor and from said direction-of-gravity reference, wherein said processor runs a program for determining a bias error correction for said angular rate sensor while said angular rate sensor is in said first position and for using said bias error correction to correct angular rate determined by said angular rate sensor while said angular rate sensor is in said second position.

37. A sensing unit as recited in claim 36, wherein said direction-of-gravity reference includes three substantially orthogonal accelerometers and wherein said angular rate sensor is one of three substantially orthogonal angular rate sensors.

38. A sensing unit as recited in claim 36, wherein said processor moves with said angular rate sensor.

39. A sensing unit as recited in claim 36, wherein said processor is mounted separate from said angular rate sensor.