METHOD AND/OR SYSTEM FOR SELECTIVE APPLICATION OF DIRECTION OF TRAVEL

• US 20140288824A1
• Filed: 11/15/2013
• Published: 09/25/2014
• Est. Priority Date: 03/22/2013
• Status: Abandoned Application

• Current Assignee: Qualcomm, Inc.
• Original Assignee: Qualcomm, Inc.
• Inventors: Czompo, Joseph, Huttunen, Tero H.
• Application Number:
  US14/082,056
• Publication Number:
  US 20140288824A1
• Time in Patent Office: Days
• US Class Current: 701/472
• CPC Class Codes: G01C 21/1654 with electromagnetic compass
• CPC Class Codes: G01C 21/1656 with passive imaging devices, e.g. cameras
• CPC Class Codes: G01S 19/47 the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial

Abstract

Described are a system, method and apparatus for computing a navigation solution. In a particular implementation, a direction of travel (DOT) indicator or vector may be applied to augment computation of the navigation solution. The DOT indicator or vector may be selectively applied in the computation of the navigation solution based, at least in part, on an assessment of reliability of the DOT indicator or vector.

Claims

1. A method, at a mobile device, comprising:

obtaining a direction of travel (DOT) indicator or vector; and

combining measurements to compute a navigation solution, wherein combining said measurements further comprises selectively applying said DOT indicator or vector in computing said navigation solution based, at least in part, on an assessment of reliability of said DOT indicator or vector.

2. The method of claim 1, wherein said measurements are obtained, at least in part, by acquisition of at least one satellite positioning system (SPS) signal.

3. The method of claim 2, wherein said measurements further comprise measurements provided by one or more inertial sensors.

4. The method of claim 1, wherein said DOT indicator or vector is selectively applied based, at least in part, on a fault detection indication computed based, at least in part, on computation of a current navigation solution without use of past DOT indicators or vectors.

5. The method of claim 1, wherein said DOT indicator or vector is selectively applied based, at least in part, on a magnitude of an uncertainty metric, and further comprising increasing said magnitude in response to detection of a turn based on one or more gyroscope measurements.

6. The method of claim 1, and further comprising:

computing a weighted mean heading based, at least in part, on multiple heading indications;

dividing a difference between the weighted mean heading and the DOT indicator or vector by a measure of an uncertainty of the weighted mean heading; and

comparing said divided difference with a rejection threshold to determine whether said DOT indicator or vector is to be applied in computation of the navigation solution.

7. The method of claim 1, and further comprising:

increasing an uncertainty metric associated with the DOT indicator or vector in response to an indication of an approaching intersection; and

selectively applying said DOT indicator or vector in computing said navigation solution based, at least in part, on said increased uncertainty metric.

8. A mobile device comprising:

a receiver to receive radio frequency signals; and

a processor to;

obtain a direction of travel (DOT) indicator or vector; and

combine measurements obtained from said received radio frequency signals to compute a navigation solution, wherein combining said measurements further comprises selectively applying said DOT indicator or vector in computing said navigation solution based, at least in part, on an assessment of reliability of said DOT indicator or vector.

9. The mobile device of claim 8, wherein said measurements are obtained, at least in part, by acquisition of at least one satellite positioning system (SPS) signal.

10. The mobile device of claim 9, wherein said measurements further comprise measurements provided by one or more inertial sensors.

11. The mobile device of claim 8, wherein said DOT indicator or vector is selectively applied based, at least in part, on a fault detection indication computed based, at least in part, on computation of a current navigation solution without use of past DOT indicators or vectors.

12. The mobile device of claim 8, wherein said DOT indicator or vector is selectively applied based, at least in part, on a magnitude of an uncertainty metric, and further comprising increasing said magnitude in response to detection of a turn based on one or more gyroscope measurements.

13. The mobile device of claim 8, wherein said processor is further to:

compute a weighted mean heading based, at least in part, on multiple heading indications;

divide a difference between the weighted mean heading and the DOT indicator or vector by a measure of an uncertainty of the weighted mean heading; and

compare said divided difference with a rejection threshold to determine whether said DOT indicator or vector is to be applied in computation of the navigation solution.

14. The mobile device of claim 8, wherein said processor is further to:

increase an uncertainty metric associated with the DOT indicator or vector in response to an indication of an approaching intersection; and

selectively apply said DOT indicator or vector in computing said navigation solution based, at least in part, on said increased uncertainty metric.

15. An apparatus for managing a navigation process on a mobile device, comprising:

means for obtaining a direction of travel (DOT) indicator or vector; and

means for combining measurements to compute a navigation solution, wherein combining said measurements further comprises selectively applying said DOT indicator or vector in computing said navigation solution based, at least in part, on an assessment of reliability of said DOT indicator or vector.

16. The apparatus of claim 15, wherein said measurements are obtained, at least in part, by acquisition of at least one satellite positioning system (SPS) signal.

17. The apparatus of claim 16, wherein said measurements further comprise measurements provided by one or more inertial sensors.

18. The apparatus of claim 15, wherein said DOT indicator or vector is selectively applied based, at least in part, on a fault detection indication computed based, at least in part, on computation of a current navigation solution without use of past DOT indicators or vectors.

19. The apparatus of claim 15, wherein said DOT indicator or vector is selectively applied based, at least in part, on a magnitude of an uncertainty metric, and further comprising increasing said magnitude in response to detection of a turn based on one or more gyroscope measurements.

20. The apparatus of claim 15, and further comprising:

means for computing a weighted mean heading based, at least in part, on multiple heading indications;

means for dividing a difference between the weighted mean heading and the DOT indicator or vector by a measure of an uncertainty of the weighted mean heading; and

means for comparing said divided difference with a rejection threshold to determine whether said DOT indicator or vector is to be applied in computation of the navigation solution.

21. The apparatus of claim 15, and further comprising:

means for increasing an uncertainty metric associated with the DOT indicator or vector in response to an indication of an approaching intersection; and

means for selectively applying said DOT indicator or vector in computing said navigation solution based, at least in part, on said increased uncertainty metric.

22. An article comprising:

a non-transitory storage medium comprising machine-readable instructions stored thereon which are executable by a special purpose computing apparatus to;

obtain a direction of travel (DOT) indicator or vector; and

combine measurements to compute a navigation solution, wherein combining said measurements further comprises selectively applying said DOT indicator or vector in computing said navigation solution based, at least in part, on an assessment of reliability of said DOT indicator or vector.

23. The article of claim 22, wherein said measurements are obtained, at least in part, by acquisition of at least one satellite positioning system (SPS) signal.

24. The article of claim 23, wherein said measurements further comprise measurements provided by one or more inertial sensors.

25. The article of claim 22, wherein said DOT indicator or vector is selectively applied based, at least in part, on a fault detection indication computed based, at least in part, on computation of a current navigation solution without use of past DOT indicators or vectors.

26. The article of claim 22, wherein said DOT indicator or vector is selectively applied based, at least in part, on a magnitude of an uncertainty metric, and further comprising increasing said magnitude in response to detection of a turn based on one or more gyroscope measurements.

27. The article of claim 22, wherein said instructions are further executable by said special purpose computing apparatus to:

compute a weighted mean heading based, at least in part, on multiple heading indications;

divide a difference between the weighted mean heading and the DOT indicator or vector by a measure of an uncertainty of the weighted mean heading; and

compare said divided difference with a rejection threshold to determine whether said DOT indicator or vector is to be applied in computation of the navigation solution.

28. The article of claim 22, wherein said instructions are further executable by said special purpose computing apparatus to:

increase an uncertainty metric associated with the DOT indicator or vector in response to an indication of an approaching intersection; and

selectively apply said DOT indicator or vector in computing said navigation solution based, at least in part, on said increased uncertainty metric.