Unassisted indoor GPS receiver

• US 7,570,208 B2
• Filed: 12/29/2005
• Issued: 08/04/2009
• Est. Priority Date: 12/29/2005
• Status: Active Grant

• Current Assignee: Samsung Electronics Co. Ltd.
• Original Assignee: SIRF Technology Incorporated (Qualcomm, Inc.)
• Inventors: Wang, Chi-Shin, Mo, Jun, Qiu, Zongde, Kudrethaya, Shridhara A.
• Primary Examiner(s): Issing; Gregory C
• Application Number:
  US11/324,144
• Publication Number:
  US 20070152878A1
• Time in Patent Office: 1,314 Days
• Field of Search: 342/357.12, 342/357.15, 455/343.2
• US Class Current: 342/357.63
• CPC Class Codes: G01S 19/24 Acquisition or tracking or demodulation of signals transmitted by the system synchronisation aspects of direct sequence spread spectrum modulation H04B1/7073
• CPC Class Codes: G01S 19/246 involving long acquisition integration times, extended snapshots of signals or methods specifically directed towards weak signal acquisition
• CPC Class Codes: G01S 19/27 creating, predicting or correcting ephemeris or almanac data within the receiver
• CPC Class Codes: G01S 19/29 carrier including Doppler, related G01S19/246 takes precedence
• CPC Class Codes: G01S 19/34 Power consumption

Abstract

The present invention provides GPS receivers capable of tracking very weak GPS signals particularly in an indoor environment without assistance from an external server or a network. In a preferred embodiment, a GPS receiver initially acquires and locks onto GPS satellite signals to compute receiver position outdoors. The GPS receiver then tracks at least one satellite signal indoors to maintain acquisition parameters for quick acquisition of GPS signals. To save power, the receiver automatically goes to the sleep state and periodically wakes up, i.e., powers up, to maintain the at least one satellite signal tracking. During the wakeup state, the receiver collects ephemeris data from the at least one satellite signal when the ephemeris data needs to be updated for quick acquisition of GPS signals.

Claims

1. A method for operating a satellite-based navigational receiver under weak signal conditions, comprising:

switching the receiver between a sleep state with a portion of the satellite-based navigation receiver powered down and a wake-up state where the receiver has access to first ephemeris data;

predicting first position information for an at least one satellite using polynomial extrapolation based upon at least the first ephemeris data;

acquiring at least one satellite signal during the wake-up state using at least the predicted first position information, if the receiver is unable to acquire the at least one satellite signal during the wake up state, switching the receiver to the sleep state and reattempting to reacquire the at least one satellite signal after a predetermined period using at least the predicted first position information; and

attempting to collect second ephemeris data from the at least one satellite signal acquired during the wake-up state.

2. The method of claim 1, further comprising using the first ephemeris data from the at least one satellite signal to synchronize a receiver clock with GPS time.

3. The method of claim 1, wherein the long integration comprises long coherent integration.

4. The method of claim 1, wherein the long integration comprises long non-coherent integration.

5. The method of claim 1, wherein time durations of the long integration depend on signal-to-noise ratios of the satellite signals.

6. The method of claim 1, wherein a period of the sleep state is in the range of (720 to 730 seconds)*n, where n is an integer and a period of the wakeup state is in the range of 18 to 30 seconds.

7. The method of claim 1, further comprising switching to a new satellite signal when the receiver can no longer track the at least one satellite signal.

8. The method of claim 1, wherein extracting the first ephemeris data further comprises extracting the first ephemeris data by overlaying a plurality of sequential data frames in the at least one satellite signal.

9. The method of claim 8, wherein the receiver has in-phase and Quadrature paths, and the sequential navigation frames are overlaid in both the in-phase and Quadrature paths.

10. The method of claim 8, further comprising using preambles in the data frames to correctly overlay the plurality of sequential data frames.

11. The method of claim 8, further comprising using predetermined words in the data frames to correctly overlay the plurality of sequential data frames.

12. The method of claim 8, wherein the number of data frames depends on the signal-to-noise ratio of the at least one satellite signal.

13. The method of claim 1, wherein extracting the first ephemeris data further comprises extracting the ephemeris data based on a majority voting decision of a plurality of sequential data frames in the at least one satellite signal.

14. The method of claim 1, further comprising using almanac data when the first ephemeris data is unavailable.

15. The method of claim 1, wherein the tracking of the at least one satellite signal occurs when the receiver is operating indoors.

16. The method of claim 1, wherein acquiring the satellite signals using the long integration further comprises:

extending the long integration over a duration of several navigation data bits; and

assuming at least one of a preamble, a hand-over word (HOW), and a week number to facilitate acquisition of the satellite signals.

17. The method of claim 16, further comprising:

establishing a threshold value for the long integration; and

identifying the at least one of the preamble, the HOW word, and the week number when the long integration has a value greater than the threshold value.

18. The method of claim 16, further comprising synchronizing the long integration to the at least one of the preamble, the HOW word, and the week number by integrating several times at predetermined time intervals, the predetermined time intervals being a repeat time of the at least one of the preamble, the HOW word, and the week number.

19. The method of claim 1, further comprising using a frequency domain technique to handle wide frequency variations due to high dynamics.

20. The method of claim 19, wherein the frequency domain technique comprises computing a Fast Fourier Transform.

21. The method of claim 20, wherein the Fast Fourier Transform computation is based on a sliding window.

22. The method of claim 1, further comprising predicting the ephemeris data when the ephemeris data is unavailable.

23. The method of claim 1, wherein the long integration is long coherent integration and navigation data is used to facilitate the long coherent integration.

24. The method of claim 1, wherein the satellite signals are transmitted from GPS satellites.

25. The method of claim 1, wherein the satellite signals are transmitted from a GLONASS or Galileo navigational system.

26. A navigational receiver, comprising:

a radio frequency front-end for receiving satellite signals;

a baseband section for processing the received satellite signals into correlated values; and

a processor adapted to;

switch the receiver between a sleep state with a portion of the satellite-based navigation receiver powered down and a wakeup state, where the receiver has access to first ephemeris data;

predict first position information for an at least one satellite using polynomial extrapolation based upon at least the first ephemeris data;

acquire at least one satellite signal during the wake-up state using at least the predicted first position information, if the processor is unable to acquire the at least one satellite signal during the wake up state, switch the radio frequency front-end to the sleep state and reattempt to reacquire the at least one satellite signal after a predetermined period using at least the predicted first position information;

attempt to collect second ephemeris data from the at least one satellite signal during the wake-up state.

27. The navigational receiver of claim 26, wherein the processor computes receiver position indoors and stores the receiver position in memory.

28. The navigational receiver of claim 27, wherein the processor computes acquisition parameters from the collected first ephemeris data and stored receiver position.

29. The navigational receiver of claim 26, wherein the processor performs long coherent integration on the correlated values.

30. The navigational receiver of claim 28, wherein time durations of the long integration depend on signal-to-noise ratios of the satellite signals.

31. The navigational receiver of claim 26, wherein a period of the sleep state is in the range of (720 to 730 seconds)*n, where n is an integer and a period of the wakeup state is in the range of 18 to 30 seconds.

32. The navigational receiver of claim 26, wherein the processor switches to a new satellite signal when the receiver can no longer track the at least one satellite signal.

33. The navigational receiver of claim 26, wherein the processor extracts the first ephemeris data by overlaying a plurality of sequential data frames in the at least one satellite signal.

34. The navigational receiver of claim 33, wherein the baseband section has in-phase and Quadrature paths, and the processor overlays the sequential navigation frames both the in-phase and Quadrature paths.

35. The navigational receiver of claim 33, wherein the processor uses preambles in the data frames to correctly overlay the plurality of sequential data frames.

36. The navigational receiver of claim 33, wherein the processor uses predetermined words in the data frames to correctly overlay the plurality of sequential data frames.

37. The navigational receiver of claim 33, wherein the number of data frames depends on the signal-to-noise ratio of the at least one satellite signal.

38. The navigational receiver of claim 26, wherein the processor extracts the first ephemeris data based on a majority voting decision of a plurality of sequential data frames in the at least one satellite signal.

39. The navigational receiver of claim 26, wherein the processor uses almanac data when the first ephemeris data is unavailable.

40. The navigational receiver of claim 26, wherein the processor tracks the at least one satellite signal when the receiver is operating indoors.

41. The navigational receiver of claim 26, wherein, in being adapted to integrate the correlated values to acquire the satellite signals, the processor is further adapted to:

integrate the correlated values over a duration of several navigation data bits; and

assume at least one of a preamble, a hand-over word (HOW), and a week number to facilitate acquisition of the satellite signals.

42. The navigational receiver of claim 41, wherein the processor is further adapted to:

establish a threshold value for the integration of the correlated values; and

identify that at least one of the preamble, the HOW word, and the week number when the integration of the correlated values has a value greater than the threshold value.

43. The navigational receiver of claim 41, wherein the processor synchronizes the integration of the correlated values to the at least one of the preamble, the HOW word, and the week number by integrating several times at predetermined time intervals, the predetermined time intervals being a repeat time of the at least one of the preamble, the HOW word, and the week number.

44. The navigational receiver of claim 26, wherein the processor uses a frequency domain technique to handle wide frequency variations due to high dynamics.

45. The navigational receiver of claim 44, wherein the frequency domain technique comprises computing a Fast Fourier Transform.

46. The navigational receiver of claim 45, wherein the Fast Fourier Transform computation is based on a sliding window.

47. The navigational receiver of claim 26, wherein the satellite signals are transmitted from GPS satellites.

48. The navigational receiver of claim 26, wherein the satellite signals are transmitted from a GLONASS or Galileo navigational system.