Stand alone global positioning system (GPS) and method with high sensitivity

• US 6,075,987 A
• Filed: 02/27/1998
• Issued: 06/13/2000
• Est. Priority Date: 02/27/1998
• Status: Expired due to Term

• Current Assignee: IDTP Holdings Incorporated (InterDigital, Inc.)
• Original Assignee: Ericsson, Inc. (Telefonaktiebolaget LM Ericsson)
• Inventors: Camp, Thomas O. Jr., Makovicka, Thomas J.
• Primary Examiner(s): Eisenzopf, Reinhard
• Assistant Examiner(s): MEHRPOUR, NAGHMEH
• Application Number:
  US09/032,053
• Time in Patent Office: 837 Days
• Field of Search: 455/12.1, 455/13.1, 455/13.2, 455/456, 455/457, 455/427, 455/418, 455/405, 342/357.12, 342/357.15, 701/213
• US Class Current: 455/427
• CPC Class Codes: G01S 19/05 providing aiding data
• CPC Class Codes: G01S 19/256 relating to timing, e.g. time of week, code phase, timing offset
• CPC Class Codes: G01S 19/258 relating to the satellite constellation, e.g. almanac, ephemeris data, lists of satellites in view
• CPC Class Codes: G01S 2205/008 using a mobile telephone network

Abstract

A method is provided for determining the position of a user terminal utilizing global positioning system (GPS) satellites, each of the GPS satellites transmitting a signal containing information indicative of the orbital parameters of the respective GPS satellite, timing and synchronization data and clock correction parameters. The method includes the steps of approximating an expected range of Doppler frequencies within which at least one GPS satellite should be located, within this range, searching for and acquiring a first GPS signal from a first GPS satellite at the user terminal strong enough to demodulate, the first GPS signal containing information indicative of the orbital parameters of the first GPS satellite, timing and synchronization data and clock correction parameters, demodulating the first GPS signal to obtain time of week information, measuring code phase synchronization for the first GPS signal utilizing the time of week information, searching for and acquiring second, third and fourth GPS signals at the user terminal from second, third and fourth GPS satellites, respectively, measuring code phase synchronizations for the second, third and fourth GPS signals utilizing the time of week information, and calculating the position of the user terminal utilizing the code phase synchronizations of the first through fourth GPS signals.

Claims

1. A method for determining the position of a user terminal utilizing global positioning system (GPS) satellites, each of the GPS satellites transmitting a signal containing information indicative of the orbital parameters of the respective GPS satellite, timing and synchronization data and clock correction parameters, said method comprising the steps of:

approximating an expected range of Doppler frequencies within which at least one GPS satellite should be located;

within this range, searching for and acquiring a first GPS signal from a first GPS satellite at the user terminal strong enough to demodulate, the first GPS signal containing information indicative of the orbital parameters of the first GPS satellite, timing and synchronization data and clock correction parameters;

demodulating the first GPS signal to obtain time of week information;

measuring code phase synchronization for the first GPS signal utilizing the time of week information;

searching for and acquiring second, third and fourth GPS signals at the user terminal from second, third and fourth GPS satellites, respectively;

measuring code phase synchronizations for the second, third and fourth GPS signals utilizing the time of week information; and

calculating the position of the user terminal utilizing the code phase synchronizations of the first through fourth GPS signals.

2. The method of claim 1, wherein the step of approximating an expected range of Doppler frequencies within which at least one GPS satellite should be located comprises the steps of:

approximating an orbital location of the at least one GPS satellite;

approximating a ground location of the user terminal with respect to a location remote from the user terminal; and

using the orbital and ground location approximations to calculate the expected range of Doppler frequencies.

3. The method of claim 2, wherein the step of approximating an orbital location of the at least one GPS satellite comprises the steps of:

receiving orbital parameters and clock correction data of the at least one GPS satellite at the user terminal from a communications system remote from the user terminal; and

using the orbital parameters and clock correction data to calculate the approximate orbital location of the at least one GPS satellite.

4. The method of claim 2, wherein the step of approximating an orbital location of the at least one GPS satellite comprises the steps of:

testing orbital parameters and clock correction data of the at least one GPS satellite, which have been retained at the user terminal from a previous communication, to see if the retained orbital parameters and clock correction data are sufficiently current;

if the retained orbital parameters and clock correction data are determined to be sufficiently current, using the retained orbital parameters and clock correction data to calculate the approximate orbital location of the at least one GPS satellite; and

if the retained orbital parameters and clock correction data are determined to not be sufficiently current,

requesting and receiving, from a communications system remote from the user terminal, current orbital parameters and clock correction data of the at least one GPS satellite at the user terminal; and

using the current orbital parameters and clock correction data to calculate the approximate orbital location of the at least one GPS satellite.

5. The method of claim 4, wherein the retained orbital parameters and clock correction data are considered sufficiently current if they are less than four hours old from time of issue.

6. The method of claim 2, wherein the step of approximating a ground location of the user terminal with respect to a location remote from the user terminal comprises the step of:

communicating with a communications system remote from the user terminal to determine approximately the ground location of the user terminal with respect to a base station included in the communications system, said base station having a known location.

7. The method of claim 6, wherein the base station comprises a cellular base station.

8. The method of claim 1, wherein the step of searching for and receiving second, third and fourth GPS signals at the user terminal from second, third and fourth GPS satellites, respectively, comprises the steps of:

approximating an expected range of Doppler frequencies within which the second, third and fourth GPS satellites should be located; and

within this range, searching for and acquiring the second, third and fourth GPS signals at the user terminal from the second, third and fourth GPS satellites, respectively.

9. The method of claim 8, wherein the step of approximating an expected range of Doppler frequencies within which the second, third and fourth GPS satellites should be located comprises the steps of:

approximating orbital locations of the second, third and fourth GPS satellites;

approximating a ground location of the user terminal with respect to a location remote from the user terminal; and

using the orbital and ground location approximations to calculate the expected range of Doppler frequencies.

10. The method of claim 9, wherein the step of approximating orbital locations of the second, third and fourth GPS satellites comprises the steps of:

receiving orbital parameters and clock correction data of the second, third and fourth GPS satellites at the user terminal from a communications system remote from the user terminal; and

using the orbital parameters and clock correction data to calculate the approximate orbital locations of the second, third and fourth GPS satellites.

11. The method of claim 9, wherein the step of approximating orbital locations of the second, third and fourth GPS satellites comprises the steps of:

testing orbital parameters and clock correction data of the second, third and fourth GPS satellites, which have been retained at the user terminal from a prior communication, to see if the retained orbital parameters and clock correction data are sufficiently current;

if the retained orbital parameters and clock correction data are determined to be sufficiently current, using the retained orbital parameters and clock correction data to calculate the approximate orbital locations of the second, third and fourth GPS satellites; and

if the retained orbital parameters and clock correction data are determined to not be sufficiently current,

requesting and receiving, from a communications system remote from the user terminal, current orbital parameters and clock correction data of the second, third and fourth GPS satellites at the user terminal; and

using the current orbital parameters and clock correction data to calculate the approximate locations of the second, third and fourth GPS satellites.

12. The method of claim 11, wherein the retained orbital parameters and clock correction data are considered sufficiently current if they are less than four hours old from time of issue.

13. The method of claim 9, wherein the step of approximating a ground location of the user terminal with respect to a location remote from the user terminal comprises the step of:

communicating with a communications system remote from the user terminal to determine approximately the ground location of the user terminal with respect to a base station included in the communications system, said base station having a known location.

14. The method of claim 13, wherein the base station comprises a cellular base station.

15. The method of claim 8, wherein the step of searching for and acquiring second, third and fourth GPS signals at the user terminal from second, third and fourth GPS satellites, respectively, further comprises the steps of:

approximating an expected range of code phase space within which the second, third and fourth GPS satellites should be located; and

within this range, searching for and acquiring the second, third and fourth GPS signals at the user terminal from the second, third and fourth GPS satellites, respectively.

16. The method of claim 15, wherein the steps of searching for and acquiring the second, third and fourth GPS signals comprises the step of:

performing long coherent integration to search for and acquire the second, third and fourth GPS signals from the second, third and fourth GPS satellites, respectively.

17. The method of claim 15, wherein the step of approximating an expected range of code phase space within which the second, third and fourth GPS satellites should be located comprises the steps of:

approximating orbital locations of the second, third and fourth GPS satellites;

refining the orbital location approximations utilizing the time of week information;

approximating a ground location of the user terminal with respect to a location remote from the user terminal; and

using the ground and refined orbital approximations to calculate the expected range of code phase space.

18. A method for determining the position of a user terminal utilizing global positioning system (GPS) satellites, each of the GPS satellites transmitting a signal containing information indicative of the orbital parameters of the respective GPS satellite, timing and synchronization data and clock correction parameters, said method comprising the steps of:

approximating an expected range of Doppler frequencies within which at least one GPS satellite should be located;

within this range, searching for a first GPS satellite signal strong enough to demodulate;

if the first GPS satellite signal strong enough to demodulate is located, acquiring and demodulating the first GPS satellite signal to obtain time of week information;

if the first GPS satellite signal strong enough to demodulate cannot be located, acquiring the first GPS satellite signal at the user terminal and utilizing a real time clock at the user terminal to approximate time of week information;

measuring code phase synchronization for the first GPS satellite signal utilizing the time of week information;

searching for and acquiring second, third and fourth GPS satellite signals at the user terminal from second, third and fourth GPS satellites, respectively;

measuring code phase synchronizations for the second, third and fourth GPS satellite signals utilizing the time of week information; and

calculating the position of the user terminal utilizing the code phase synchronizations of the first through fourth GPS satellite signals.

19. The method of claim 18, wherein the real time clock at the user terminal is periodically updated by:

searching for and acquiring a GPS satellite signal at the user terminal having a sufficient signal level to demodulate; and

demodulating the acquired GPS satellite signal to obtain time of week information, wherein the real time clock at the user terminal is updated with the obtained time of week information.

20. The method of claim 18, further comprising the step of:

if the first GPS satellite signal is strong enough to be demodulated, updating the real time clock at the user terminal with the time of week information obtained from demodulating the first GPS satellite signal.

21. The method of claim 18, wherein the real time clock at the user terminal is utilized to approximate the time of week information regardless of whether the first GPS satellite signal is strong enough to demodulate.

22. The method of claim 18, wherein the step of approximating an expected range of Doppler frequencies within which at least one GPS satellite should be located comprises the steps of:

approximating an orbital location of the at least one GPS satellite;

approximating a ground location of the user terminal with respect to a location remote from the user terminal; and

using the orbital and ground location approximations to calculate the expected range of Doppler frequencies.

23. The method of claim 22, wherein the step of approximating an orbital location of the at least one GPS satellite comprises the steps of:

receiving orbital parameters and clock correction data of the at least one GPS satellite at the user terminal from a communications system remote from the user terminal; and

using the orbital parameters and clock correction data to calculate the approximate orbital location of the at least one GPS satellite.

24. The method of claim 22, wherein the step of approximating an orbital location of the at least one GPS satellite comprises the steps of:

testing orbital parameters and clock correction data of the at least one GPS satellite, which have been retained at the user terminal from a previous communication, to see if the retained orbital parameters and clock correction data are sufficiently current;

if the retained orbital parameters and clock correction data are determined to be sufficiently current, using the retained orbital parameters and clock correction data to calculate the approximate orbital location of the at least one GPS satellite; and

if the retained orbital parameters and clock correction data are determined to not be sufficiently current,

requesting and receiving, from a communications system remote from the user terminal, current orbital parameters and clock correction data of the at least one GPS satellite at the user terminal; and

using the current orbital parameters and clock correction data to calculate the approximate orbital location of the at least one GPS satellite.

25. The method of claim 24, wherein the retained orbital parameters and clock correction data are considered sufficiently current if they are less than four hours old from time of issue.

26. The method of claim 22, wherein the step of approximating a ground location of the user terminal with respect to a location remote from the user terminal comprises the step of:

communicating with a communications system remote from the user terminal to determine approximately the ground location of the user terminal with respect to a base station included in the communications system, said base station having a known location.

27. The method of claim 26, wherein the base station comprises a cellular base station.

28. The method of claim 18, wherein the step of searching for and receiving second, third and fourth GPS signals at the user terminal from second, third and fourth GPS satellites, respectively, comprises the steps of:

approximating an expected range of Doppler frequencies within which the second, third and fourth GPS satellites should be located; and

within this range, searching for and acquiring the second, third and fourth GPS signals at the user terminal from the second, third and fourth GPS satellites, respectively.

29. The method of claim 28, wherein the step of approximating an expected range of Doppler frequencies within which the second, third and fourth GPS satellites should be located comprises the steps of:

approximating orbital locations of the second, third and fourth GPS satellites;

approximating a ground location of the user terminal with respect to a location remote from the user terminal; and

using the orbital and ground location approximations to calculate the expected range of Doppler frequencies.

30. The method of claim 29, wherein the step of approximating orbital locations of the second, third and fourth GPS satellites comprises the steps of:

receiving orbital parameters and clock correction data of the second, third and fourth GPS satellites at the user terminal from a communications system remote from the user terminal; and

using the orbital parameters and clock correction data to calculate the approximate orbital locations of the second, third and fourth GPS satellites.

31. The method of claim 29, wherein the step of approximating orbital locations of the second, third and fourth GPS satellites comprises the steps of:

testing orbital parameters and clock correction data of the second, third and fourth GPS satellites, which have been retained at the user terminal from a prior communication, to see if the retained orbital parameters and clock correction data are sufficiently current;

if the retained orbital parameters and clock correction data are determined to be sufficiently current, using the retained orbital parameters and clock correction data to calculate the approximate orbital locations of the second, third and fourth GPS satellites; and

if the retained orbital parameters and clock correction data are determined to not be sufficiently current,

requesting and receiving, from a communications system remote from the user terminal, current orbital parameters and clock correction data of the second, third and fourth GPS satellites at the user terminal; and

using the current orbital parameters and clock correction data to calculate the approximate locations of the second, third and fourth GPS satellites.

32. The method of claim 31, wherein the retained orbital parameters and clock correction data are considered sufficiently current if they are less than four hours old from time of issue.

33. The method of claim 29, wherein the step of approximating a ground location of the user terminal with respect to a location remote from the user terminal comprises the step of:

communicating with a communications system remote from the user terminal to determine approximately the ground location of the user terminal with respect to a base station included in the communications system, said base station having a known location.

34. The method of claim 33, wherein the base station comprises a cellular base station.

35. The method of claim 28, wherein the step of searching for and acquiring second, third and fourth GPS signals at the user terminal from second, third and fourth GPS satellites, respectively, further comprises the steps of:

approximating an expected range of code phase space within which the second, third and fourth GPS satellites should be located; and

within this range, searching for and acquiring the second, third and fourth GPS signals at the user terminal from the second, third and fourth GPS satellites, respectively.

36. The method of claim 35, wherein the steps of searching for and acquiring the second, third and fourth GPS signals comprises the step of:

performing long coherent integration to search for and acquire the second, third and fourth GPS signals from the second, third and fourth GPS satellites, respectively.

37. The method of claim 35, wherein the step of approximating an expected range of code phase space within which the second, third and fourth GPS satellites should be located comprises the steps of:

approximating orbital locations of the second, third and fourth GPS satellites;

refining the orbital location approximations utilizing the time of week information;

approximating a ground location of the user terminal with respect to a location remote from the user terminal; and

using the ground and refined orbital approximations to calculate the expected range of code phase space.