Apparatus and method for maintaining time synchronization in AGPS receiver

• US 20060170589A1
• Filed: 01/27/2006
• Published: 08/03/2006
• Est. Priority Date: 01/28/2005
• Status: Abandoned Application

• Current Assignee: Samsung Electronics Co. Ltd.
• Original Assignee: Samsung Electronics Co. Ltd.
• Inventors: Park, Chan-Woo, Choi, Sun, Park, Ki-Hyun
• Application Number:
  US11/340,610
• Publication Number:
  US 20060170589A1
• Time in Patent Office: Days
• US Class Current: 342/357.640
• CPC Class Codes: G01S 19/25 involving aiding data received from a cooperating element, e.g. assisted GPS

Abstract

An apparatus and method are provided for obtaining a location of a CDMA personal portable terminal according to an AGPS scheme. The method includes receiving a Doppler value of a satellite from an AGPS server, receiving a satellite signal and measuring a Doppler value of the satellite by using the received satellite signal, calculating a code frequency bias ψ_b by using a difference between the received Doppler value and the measured Doppler value, calculating a code bias φ_b in consideration of the calculated code frequency bias ψ_b and a search duration, and calculating a pseudorange of the satellite by compensating for the calculated code bias φ_b.

Claims

1. A global positioning apparatus of a personal portable terminal which uses an Assisted Global Positioning System (AGPS) scheme in a Code Division Multiple Access (CDMA) communication system, the global positioning apparatus comprising:

a reference clock for providing a reference frequency;

a CDMA baseband processor for processing signals transmitted to and received from a CDMA base station;

a GPS baseband processor for processing GPS baseband signals transmitted to and received from a GPS satellite;

an AGPS message receiver unit for receiving a Doppler value of a GPS signal from an AGPS server in order to scan at least one GPS satellite signal;

an operation part for performing an operation for an estimation of a location of the personal portable terminal, receiving the GPS signal, and measuring a Doppler value of the GPS signal; and

a processing part for calculating a time error by using results of the operation by the operation part and obtaining a pseudorange from the GPS satellite by using the calculated time error.

2. The global positioning apparatus as claimed in claim 1, wherein the operation part comprises:

a memory for storing a correlation result output from the GPS baseband processor and a result of a Fast Fourier Transform (FFT); and

an FFT unit for performing the FFT in order to obtain an expected reference Doppler frequency for each satellite.

3. The global positioning apparatus as claimed in claim 2, wherein the result of the FFT is stored in the memory and has a Doppler measurement resolution of about 1000/n Hz.

4. The global positioning apparatus as claimed in claim 2, wherein the FFT unit is configured to perform the FFT in order to maintain an accuracy of the Doppler bias value.

5. The global positioning apparatus as claimed in claim 1, wherein the processing part comprises:

a signal detector for detecting GPS satellites exceeding a predetermined signal detection threshold by comparing magnitudes of resultant signals of the FFT with the signal detection threshold;

a reference frequency error measurer for measuring Doppler frequencies of the GPS satellites detected by the signal detector, measuring Doppler biases which are differences between the measured Doppler frequencies and reference Doppler frequencies estimated for each satellite by the AGPS message receiver unit, and generating a code frequency bias by using the measured common Doppler bias;

a time error calculator for calculating a time error as a code phase error by using the code frequency bias value;

a time error compensator for compensating for the time error calculated by the time error calculator;

a signal processor for generating a pseudorange between the personal portable terminal and each satellite by using code phase measurements of signals detected by the signal detector, and compensating for the time error input from the time error compensator when generating the pseudorange; and

a measured result transmitter for transmitting to the AGPS server a resultant pseudorange obtained through compensation of the time error by the signal processor.

6. The global positioning apparatus as claimed in claim 1, wherein the Doppler bias corresponds to a difference between a Doppler frequency of a GPS satellite detected and measured by the signal detector, and a reference Doppler frequency estimated for each satellite by the AGPS message receiver unit.

7. The global positioning apparatus as claimed in claim 5, wherein the Doppler bias is determined by a bias of a reference frequency generated by the reference clock.

8. The global positioning apparatus as claimed in claim 5, wherein the Doppler bias induces a bias in a frequency of a local oscillator within the GPS RF processor which down-converts GPS RF signals.

9. The global positioning apparatus as claimed in claim 5, wherein the Doppler bias is determined by user'"'"'s motion.

10. The global positioning apparatus as claimed in claim 9, wherein the Doppler bias due to the user'"'"'s motion for a predetermined satellite i corresponds to a sum of a local oscillator bias and a user Doppler value for the satellite i as defined by the following equation,

Doppler bias(i)=LO bias+user Doppler(i).

11. The global positioning apparatus as claimed in claim 5, wherein the local bias corresponds to a difference between a Doppler frequency of a satellite detected by the signal detector, and a Doppler frequency estimated for each satellite by the AGPS message receiver unit, and the difference is used as one common Doppler bias value by the satellites.

12. The global positioning apparatus as claimed in claim 5, wherein the code frequency bias ψ

_b is calculated by the following equation,

ψ

_b=D_b×

k[chips/sec],

wherein D_b denotes the Doppler bias and k denotes a value obtained by dividing a code frequency by a carrier frequency.

13. The global positioning apparatus as claimed in claim 5, wherein the code bias φ

_b is calculated by the following equation,

φ

_b=ψ

_b×

t_GPS,

wherein ψ

_b denotes a code frequency bias and t_GPS denotes search duration.

14. A method for global positioning of a personal portable terminal which uses an Assisted Global Positioning System (AGPS) scheme in a Code Division Multiple Access (CDMA) communication system, the method comprising the steps of:

receiving a Doppler value of a satellite from an AGPS server;

receiving a satellite signal and measuring a Doppler value of the satellite by using the received satellite signal;

calculating a code frequency bias ψ

_b by using a difference between the received Doppler value and the measured Doppler value;

calculating a code bias φ

_b in consideration of the calculated code frequency bias ψ

_b and a search duration; and

calculating a pseudorange of the satellite by compensating for the calculated code bias φ

_b.

15. The method as claimed in claim 14, wherein the Doppler value obtained by the FFT has a Doppler measurement resolution of about 1000/n Hz, which is used in measuring the Doppler frequency, and the reference frequency error is calculated by using the measured Doppler frequency.

16. The method as claimed in claim 14, further comprising the step of transmitting a pseudorange of the calculated satellite to the AGPS server.

17. The method as claimed in claim 14, wherein the Doppler value obtained by the FFT corresponds to the reference Doppler value estimated for each satellite.

18. The method as claimed in claim 14, wherein a Doppler bias corresponds to a difference between a Doppler frequency measured from a GPS satellite signal and the reference Doppler frequency, and is determined by a bias of a reference frequency generated by the reference clock.

19. The method as claimed in claim 18, wherein the Doppler bias induces a bias in a frequency of a local oscillator.

20. The method as claimed in claim 18, wherein the Doppler bias is determined by user'"'"'s motion.

21. The method as claimed in claim 20, wherein the Doppler bias due to the user'"'"'s motion for a predetermined satellite i corresponds to a sum of a local oscillator bias and a user Doppler value for the satellite i as defined by the following equation,

Doppler bias(i)=LO bias+user Doppler(i).

22. The method as claimed in claim 21, wherein the local bias corresponds to a difference between a Doppler frequency of a satellite detected by the signal detector and a Doppler frequency estimated for each satellite by the AGPS message receiver unit, and the difference is used as one common Doppler bias value by the satellites.

23. The method as claimed in claim 14, wherein the code frequency bias ψ

_b is calculated by the following equation,

ψ

_b=D_b×

k[chips/sec],

wherein D_b denotes the Doppler bias and k denotes a value obtained by dividing a code frequency by a carrier frequency.

24. The method as claimed in claim 14, wherein the code bias φ

_b corresponds to a receiver time error.

25. The method as claimed in claim 14, wherein the code bias φ

_b is calculated by the following equation,

φ

_b=ψ

_b×

t_GPS,

wherein ψ

_b denotes a code frequency bias and t_GPS denotes search duration.