TIME REFERENCE SYSTEM

• US 20100188286A1
• Filed: 09/17/2009
• Published: 07/29/2010
• Est. Priority Date: 09/17/2008
• Status: Active Grant

• Current Assignee: Apple Inc.
• Original Assignee: ST-Ericcson SA (Telefonaktiebolaget LM Ericsson)
• Inventors: ANYAEGBU, Esther Olulu, FLEMING, Peter Mark, BICKERSTAFF, Jacqueline Peta, WHITWORTH, Gerald
• Granted Patent: US 8,184,046 B2
• Time in Patent Office: Days
• US Class Current: 342/357.220
• 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 19/42 Determining position

Abstract

A time reference system for generating a time reference from signals produced by a global navigation satellite constellation has a satellite signal receiver to receive and down-convert code-modulated signals from a plurality of satellites and a correlator to track and decode the down-converted signals to provide signals containing partial pseudo-range measurements for respective satellites. A data processing arrangement receives assistance data from an external source and performs data-bit synchronisation in which bit edges of a low frequency data bit stream carried by the received satellite signals are identified, to perform a preliminary position-velocity-time solution to provide an approximate time reference, and to perform auto-correlation of pre-selected data sequences in the data stream to resolve time ambiguities thereby to compute a precise time reference signal in weak received signal conditions. The pre-selected data sequences may be the repeated data preamble in the GPS navigation message constituted by the data stream.

Claims

1. A time reference system for generating a time reference from signals produced by a global navigation satellite constellation, wherein the system comprises:

a satellite signal receiver having a radio frequency stage configured to receive and down convert code-modulated signals from a plurality of satellites and a correlator configured to receive, track and decode the down-converted satellite signals to provide signals containing partial pseudo-range measurements for respective satellites, and

a data processing arrangement configured to receive signals containing assistance data from a source other than the received and down-converted satellite signals and the signals containing partial pseudo-range measurements, to perform data-bit synchronisation in which the bit edges of a data bit stream carried by the received satellite signals are identified, to perform correlation of pre-selected data sequences in the data stream to resolve time ambiguities, and to compute a time reference signal based on the assistance data, the partial pseudo-range measurements and code-tracking outputs from the satellite signal receiver, the data-bit synchronisation and the data sequence correlation.

2. The system according to claim 1, including a frequency-locked loop operable to generate a Doppler shift signal indicative of Doppler shifts caused by satellite motion, wherein the data processing arrangement is configured to modify the data-bit synchronisation in response to the Doppler shift signal.

3. The system according to claim 1, wherein the data processing arrangement is configured:

(i) to provide a preliminary time solution with a time uncertainty equal to the duration of between 1 and 5 data-bits of a low frequency data stream using a position-velocity-time estimate produced from the partial pseudo-range measurements and Doppler measurements and using ambiguity resolution algorithms to provide a best-fit for the said partial pseudo-range measurements and said Doppler measurements and the assistance data,

(ii) to perform intermediate ambiguity resolution and time solution adjustment using the results of the data-bit synchronisation and the correlation of pre-selected data sequences from the signals received from a selected one of the satellites from which the receiver receives signals, and

(iii) to further adjust the time solution in response to the code-tracking outputs to produce the time reference signal.

4. The system according to claim 1, wherein the pre-selected data sequences embody a repeated data pattern, and the data processing arrangement is configured such that the correlation of the data sequences comprises correlation of successive instances of the repeated data pattern in the data stream in the signal received from at least one of the satellites from which signals are received by the receiver.

5. The system according to claim 1, wherein the pre-selected data sequences are selected on the fly using the assistance data, and/or by prediction based on previously received data sequences, and wherein the data processing arrangement is configured to perform the selection by performing auto-correlation of the data patterns of potential data sequences, the selection being based on the quality of the auto-correlation maximum compared to average or secondary values.

6. The system according to claim 4, wherein the correlation of the data sequences is performed by a combination of coherent integrations and incoherent integrations.

7. The system according to claim 1, wherein the data processing arrangement is configured to provide a preliminary position-velocity-time solution having a time accuracy no better than +/−

11 ms, the solution being in the form of a plurality of pseudo-range time-of-transmission solution options at least one of which has a time accuracy of better than ±

3 ms.

8. The system according to claim 1 further comprising a frequency-locked loop, wherein the data processing arrangement is configured to perform the correlation of the pre-selected data sequences using coherent integration over intervals no longer than a reciprocal of the frequency stability of the frequency-locked loop.

9. The system according to claim 8, wherein the data processing arrangement is configured such that the selection of the at least one option includes incoherently integrating the results of the said coherent integration over a longer interval.

10. The system according to claim 1, wherein said data sequences are pre-selected according to a predetermined correlation property.

11. The system according to claim 1, wherein the pre-selected data sequences are selected by an autocorrelation process.

12. The system according to claim 1, wherein said data sequences are pre-selected according to their performance in discriminating between alignment and misalignment of the data sequences with a reference data sequence or sequences.

13. The system according to claim 12, wherein said data sequences are pre-selected according to their auto-correlation discrimination performance.

14. A method of generating a time reference signal from signals produced by a global navigation satellite constellation, comprising:

(a) receiving, down-converting, and tracking the signals transmitted by a plurality of satellites in the constellation to produce a plurality of receiver output signals, receiving assistance data signals from a source other than the directly received satellite signals, and producing from the receiver output signals and the assistance data signals representing a preliminary time solution,

(b) correlating pre-selected data sequences, using a data processor, in a data stream carried by the signals transmitted by at least one of the satellites to resolve time ambiguities in the preliminary time solution, thereby to generate the time reference signal representing time to an accuracy of better than +/−

1 ms.

15. A method of generating a time reference signal from signals produced by a global navigation satellite constellation, comprising:

(a) receiving, down-converting, and tracking the signals transmitted by a plurality of satellites in the constellation to produce a plurality of receiver output signals, receiving assistance data signals from a source other than the directly received satellite signals, and producing from the receiver output signals and the assistance data signals representing a preliminary time solution,

(b) performing data-bit synchronization, using a data processor, in which bit edges of a data stream carried by the signals transmitted by at least one of the satellites are identified, the data-bit synchronisation including performing frequency-shift-compensated integration of samples of the received data stream.

16. A time reference system for generating a time reference signal from signals produced by a global navigation satellite constellation, wherein the system comprises:

a satellite signal receiver having a radio frequency stage for receiving and down-converting code-modulated signals from a plurality of satellites and a correlator to receive, track and decode the down-converted satellite signals to provide signals containing partial pseudo-range measurements for respective satellites, and

a data processing arrangement configured to receive signals containing assistance data from a source other than the received and down-converted satellite signals and the signals containing partial pseudo-range measurements, to perform data-bit synchronisation in which bit edges of a data bit stream carried by the received satellite signals are identified, to compute a position-velocity-time solution using time-of-arrival measurements of signals received by the receiver from the satellites, and to perform correlation of the data bit stream in the received and down-converted satellite signals with pre-selected data sequences, and, using all three of the data-bit synchronisation, the position-velocity-time solution, and the data bit stream correlation to compute a time reference signal.