APPARATUSES AND METHODS FOR TRACKING A NAVIGATION RECEIVER

• US 20140070986A1
• Filed: 11/05/2012
• Published: 03/13/2014
• Est. Priority Date: 09/10/2012
• Status: Abandoned Application

• Current Assignee: Maishi Electronic (Shanghai) Limited
• Original Assignee: O2 Micro International Limited (O2 Micro Incorporated)
• Inventors: LU, Shenghong, GAO, Ke, ZOU, Jinghua, HE, Xiaoyong
• Application Number:
  US13/669,256
• Publication Number:
  US 20140070986A1
• Time in Patent Office: Days
• US Class Current: 342/357.3
• CPC Class Codes: G01C 21/165 combined with non-inertial navigation instruments
• CPC Class Codes: G01S 19/47 the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial
• CPC Class Codes: G01S 19/52 Determining velocity
• CPC Class Codes: G01S 19/53 Determining attitude

Abstract

A satellite positioning component calculates a first position associated with a navigation receiver at a first time. An inertial positioning component calculates a second position associated with the navigation receiver at the first time. A combination positioning component provides a reference position, combines the first position and the second position into a third position based on distances among the first position, the second position, and the reference position, and locates the navigation receiver according to the third position.

Claims

1. A machine-readable medium that stores a plurality of machine-executable components for tracking a navigation receiver, said machine-executable components comprising:

a satellite positioning component that calculates a first position associated with said navigation receiver at a first time;

an inertial positioning component that calculates a second position associated with said navigation receiver at said first time; and

a combination positioning component that provides a reference position, that combines said first position and said second position into a third position based on distances between said first position, said second position, and said reference position, and that locates said navigation receiver according to said third position.

2. The machine-readable medium as claimed in claim 1, wherein said combination positioning component further comprises:

a combination unit that weights said first position and said second position to obtain weighted positions corresponding to said first position and said second position, and combines said weighted positions to generate said third position.

3. The machine-readable medium as claimed in claim 2, wherein said combination positioning component further comprises:

a weight unit that provides weight data used to weight said first and second positions, wherein said weight unit accesses a satellite flag indicating the validity of said first position, accesses an inertial flag indicating the validity of said second position, and determines said weight data according to said satellite flag and said inertial flag.

4. The machine-readable medium as claimed in claim 3, wherein said weight unit sets a combination flag to a value indicating that said third position is invalid if both said first position and said second position are invalid.

5. The machine-readable medium as claimed in claim 2, wherein said combination positioning component further comprises:

a weight unit that compares a first distance between said first position and said reference position with a threshold, that compares a second distance between said second position and said reference position with said threshold, and that provides weight data used to weight said first and second positions according to results of both said comparisons.

6. The machine-readable medium as claimed in claim 5, wherein said weight unit sets a combination flag to a value indicating that said third position is invalid if both said first distance are greater than said threshold.

7. The machine-readable medium as claimed in claim 2, wherein said combination positioning component further comprises:

a weight unit that compares a first distance between said first position and said second position with a second distance between said first position and said reference position, that compares said first distance with a third distance between said second position and said reference position, and that provides weight data used to weight said first and second positions according to results of both said comparisons.

8. The machine-readable medium as claimed in claim 7, wherein the weight of said first position is equal to said third distance divided by a sum of said second distance and said third distance if said first distance is greater than said second distance and if said first distance is greater than said third distance.

9. The machine-readable medium as claimed in claim 7, wherein the weight of said second position is equal to said second distance divided by a sum of said second distance and said third distance if said first distance is greater than said second distance and if said first distance is greater than said third distance.

10. The machine-readable medium as claimed in claim 2, wherein said combination positioning component further comprises:

a weight unit that compares a first distance between said first position and said reference position with a second distance between said second position and said reference position, and that provides weight data used to weight said first and second positions according to a result of said comparison.

11. The machine-readable medium as claimed in claim 1, wherein said machine-executable components further comprise:

a filter that accesses a combination flag indicating whether said third position is valid, and that filters said third position to obtain said location of said navigation receiver at said first time if said combination flag indicates that said third position is valid.

12. The machine-readable medium as claimed in claim 11, wherein said filter accesses location data indicating a previous location point of said navigation receiver at a second time prior to said first time, and estimates said location point at said first time according to said previous location point if said combination flag indicates that said third position is invalid.

13. The machine-readable medium as claimed in claim 12, wherein said inertial positioning component further calculates a velocity and an orientation associated with said navigation receiver at said second time, and wherein said filter estimates said location point at said first time according to said previous location point, said velocity, and said orientation if said combination flag indicates that said third position is invalid.

14. The machine-readable medium as claimed in claim 1, wherein said combination positioning component further comprises:

a reference estimator that accesses location data indicating a previous location point of said navigation receiver at a second time prior to said first time, and that estimates said reference position according to said previous location point.

15. The machine-readable medium as claimed in claim 13, wherein said satellite positioning component further calculates a first velocity and a first orientation associated with said navigation receiver at said second time, and wherein said inertial positioning component further calculates a second velocity and a second orientation associated with said navigation receiver at said second time, and wherein said reference estimator combines said first velocity and a second velocity into a third velocity, combines said first orientation and said second orientation into a third orientation, and estimates said reference position based on said previous location point, said third velocity, and said third orientation.

16. A navigation apparatus comprising:

an antenna configured to receive a plurality of satellite signals;

a plurality of motion sensors configured to provide motion signals indicating a speed and an orientation of said navigation apparatus; and

a receiver comprising a processor that executes a plurality of machine-executable components stored in a machine-readable medium to locate said navigation apparatus, wherein said machine-executable components comprise;

a satellite positioning component that calculates a first position associated with said navigation receiver at a first time according to said satellite signals;

an inertial positioning component that calculates a second position associated with said navigation receiver at said first time according to said motion signal; and

a combination positioning component that provides a reference position, that combines said first position and said second position into a third position based on distances between said first position, said second position, and said reference position, and that locates said navigation apparatus according to said third position.

17. The navigation apparatus as claimed in claim 16, wherein said combination positioning component comprises:

a combination unit that weights said first position and said second position to obtain weighted positions corresponding to said first position and said second position, and combines said weighted positions to generate said third position.

18. The navigation apparatus as claimed in claim 17, wherein said combination positioning component further comprises:

a weight unit that accesses a satellite flag indicating the validity of said first position, that accesses an inertial flag indicating the validity of said second position, and that provides weight data used to weight said first and second positions according to said satellite flag and said inertial flag.

19. The navigation apparatus as claimed in claim 18, wherein said weight unit sets a combination flag to a value indicating that said third position is invalid if both said first position and said second position are invalid.

20. The navigation apparatus as claimed in claim 17, wherein said combination positioning component further comprises:

a weight unit that compares a first distance between said first position and said reference position with a threshold, that compares a second distance between said second position and said reference position with said threshold, and that provides weight data used to weight said first and second positions according to results of both said comparisons.

21. The navigation apparatus as claimed in claim 20, wherein said weight unit sets said combination flag to a value indicating that said third position is invalid if said first distance is greater than said first threshold and if said second distance is greater than said second threshold.

22. The navigation apparatus as claimed in claim 18, wherein said combination positioning component further comprises:

a weight unit that compares a first distance between said first position and said second position with a second distance between said first position and said reference position, that compares said first distance with a third distance between said second position and said reference position, and that provides weight data used to weight said first and second positions according to results of both said comparisons.

23. The navigation apparatus as claimed in claim 18, wherein said combination positioning component further comprises:

a weight unit that compares a first distance between said first position and said reference position with a second distance between said second position and said reference position, and that provides weight data used to weight said first and second positions according to a result of said comparison.

24. The navigation apparatus as claimed in claim 16, wherein said machine-executable components further comprise:

a filter that accesses a combination flag indicating whether said third position is valid, that filters said third position to obtain said location of said navigation receiver at said first time if said combination flag indicates that said third position is valid, and that accesses location data indicating a previous location point of said navigation receiver at a second time prior to said first time, and that estimates said location at said first time according to said previous location point if said combination flag indicates that said third position is invalid.

25. The navigation apparatus as claimed in claim 16, wherein said combination positioning component further comprises:

a reference estimator that accesses location data indicating a previous location point of said navigation receiver at a second time prior to said first time, and that estimates said reference position according to said previous location point at said second time.

26. The navigation apparatus as claimed in claim 25, wherein said satellite positioning component further calculates a first velocity and a first orientation associated with said navigation receiver at said second time, and wherein said inertial positioning component further calculates a second velocity and a second orientation associated with said navigation receiver at said second time, and wherein said reference estimator combines said first velocity and a second velocity into a third velocity, combines said first orientation and said second orientation into a third orientation, and estimates said reference position based on said previous location point, said third velocity and said third orientation.

27. A navigation receiver comprising a processor that executes machine-executable instructions stored in a machine-readable medium, wherein said instructions when executed perform operations comprising:

calculating a first position associated with said navigation receiver at a first time according to a plurality of satellite signals;

calculating a second position associated with said navigation receiver at said first time according to a plurality of motion signals indicating a speed and an orientation of said navigation receiver;

providing a reference position;

combining said first position and said second position into a third position based on distances between said first position, said second position, and said reference position; and

locating said navigation receiver according to said third position.

28. The navigation receiver as claimed in claim 27, wherein said operations further comprise:

accessing weight data indicating weights of said first position and said second position;

weighting said first position and said second position based on said weight data to obtain weighted positions corresponding to said first position and said second position; and

combining said weighted positions to generate said third position.

29. The navigation receiver as claimed in claim 28, wherein said operations further comprise:

accessing a satellite flag indicating the validity of said first position;

accessing an inertial flag indicating the validity of said second position; and

determining said weight data according to said satellite flag and said inertial flag.

30. The navigation receiver as claimed in claim 29, wherein said operations further comprise:

setting a combination flag to a value indicating that said third position is invalid if both said first position and said second position are invalid.

31. The navigation receiver as claimed in claim 28, wherein said operations further comprise:

comparing a first distance between said first position and said reference position with a threshold;

comparing a second distance between said second position and said reference position with said threshold; and

determining said weight data according to results of both of said comparing operations.

32. The navigation receiver as claimed in claim 31, wherein said operations further comprise:

setting a combination flag to a value indicating that said third position is invalid if said first distance is greater than said first threshold and if said second distance is greater than said second threshold.

33. The navigation receiver as claimed in claim 28, wherein said operations further comprise:

comparing a first distance between said first position and said second position with a second distance between said first position and said reference position;

comparing said first distance with a third distance between said second position and said reference position; and

determining said weight data according to results of both of said comparing operations.

34. The navigation receiver as claimed in claim 28, wherein said operations further comprise:

comparing a first distance between said first position and said reference position with a second distance between said second position and said reference position; and

determining said weight data according to a result of said comparing operation.

35. The navigation receiver as claimed in claim 28, wherein said operations further comprise:

accessing a combination flag indicating whether said third position is valid;

filtering said third position to obtain said location of said navigation receiver if said combination flag indicates that said third position is valid;

accessing location data indicating a previous location point of said navigation receiver at a second time prior to said first time; and

estimating said location point at said first time according to said previous location point if said combination flag indicates that said third position is invalid.

36. The navigation receiver as claimed in claim 27, wherein said operations further comprise:

accessing location data indicating a previous location point of said navigation receiver at a second time prior to said first time; and

providing said reference position according to said previous location point.

37. The navigation receiver as claimed in claim 27, wherein said operations further comprise:

calculating a first velocity and a first orientation associated with said navigation receiver at said second time;

calculating a second velocity and a second orientation associated with said navigation receiver at said second time;

combining said first velocity and a second velocity into a third velocity;

combining said first orientation and said second orientation into a third orientation; and

estimating said reference position based on said previous location point, said third velocity and said third orientation.