GLOBAL NAVIGATION SATELLITE SYSTEMS (GNSS) POSITIONING USING PRECISE SATELLITE DATA

• US 20140085139A1
• Filed: 09/12/2013
• Published: 03/27/2014
• Est. Priority Date: 09/26/2012
• Status: Active Grant

• Current Assignee: Trimble Inc.
• Original Assignee: Trimble Navigation Limited (Trimble Inc.)
• Inventors: Leandro, Rodrigo, Talbot, Nicholas Charles
• Granted Patent: US 9,671,501 B2
• Time in Patent Office: Days
• US Class Current: 342/357.27
• CPC Class Codes: G01S 19/03 Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers
• CPC Class Codes: G01S 19/40 Correcting position, velocity or attitude
• CPC Class Codes: G01S 19/42 Determining position
• CPC Class Codes: G01S 19/43 using carrier phase measurements, e.g. kinematic positioning; using long or short baseline interferometry
• CPC Class Codes: G01S 19/44 Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method

Abstract

Method to estimate parameters derived at least from GNSS signals useful to determine a position, including obtaining at least one GNSS signal observed at a GNSS receiver from each of a plurality of GNSS satellites; receiving global correction information useful to correct at least the obtained GNSS signals from a first set of GNSS satellites, wherein the global correction information includes correction information which is independent from the position to be determined; receiving local correction information useful to correct at least the obtained GNSS signals from a second set of GNSS satellites, wherein the local correction information includes correction information which is dependent on the position to be determined; processing the obtained GNSS signals from the first set of GNSS satellites by using the global correction information; and processing the obtained GNSS signals from the second set of GNSS satellites by using the local correction information.

Claims

1. Method to estimate parameters derived at least from global navigational satellite system (GNSS) signals useful to determine a position, comprising:

obtaining at least one GNSS signal observed at a GNSS receiver from each of a plurality of GNSS satellites;

receiving global correction information useful to correct at least the obtained GNSS signals from a first set of GNSS satellites among the plurality of GNSS satellites, wherein the global correction information includes correction information which is independent from the position to be determined;

receiving local correction information useful to correct at least the obtained GNSS signals from a second set of GNSS satellites among the plurality of GNSS satellites, wherein the local correction information includes correction information which is dependent on the position to be determined;

processing the obtained GNSS signals from the first set of GNSS satellites by using the global correction information; and

processing the obtained GNSS signals from the second set of GNSS satellites by using the local correction information;

wherein the first set of GNSS satellites is different from the second set of GNSS satellites.

2. Method of claim 1, wherein the local correction information includes at least one of

a) observed data of a single reference receiver;

b) synthetic or semi-synthetic raw data generated for a position near the position to be determined, wherein “

near”

means at least one of;

up to a few kilometers, up to 5 kilometers, and up to 10 kilometers; and

c) raw data from a network of reference stations.

3. Method of claim 1, wherein receiving local correction information includes receiving local correction information from a local source, wherein “

local correction information from a local source”

means at least one of;

correction information generated from data of one or more receivers that are up to a few hundreds of kilometers away from the rover receiver, correction information generated from data of one or more receivers that are up to 500 kilometers away from the rover receiver, and correction information generated from data of one or more receivers that are up to 1000 kilometers away from the rover receiver.

4. Method of claim 3, wherein the local source is any one of a reference station and a reference station network.

5. Method of claim 1, wherein the global correction information includes at least one of

satellite clock correction;

satellite orbit correction; and

satellite code and phase measurement biases.

6. Method of claim 1, wherein the method uses carrier phase measurements of the GNSS signals.

7. Method of claim 6, wherein processing the obtained GNSS signals from the first set of GNSS satellites by using the global correction information includes:

inputting at least part of the global correction information to a geometry filter configured to output a candidate set of integer ambiguities.

8. Method of claim 6, wherein processing the obtained GNSS signals from the second set of GNSS satellites by using the local correction information includes:

inputting at least part of the local correction information to at least one ionospheric filter configured to output a candidate set of integer ambiguities.

9. Method of claim 6, wherein processing the obtained GNSS signals from the second set of GNSS satellites by using the local correction information includes:

inputting at least part of the local correction information to at least one code carrier filter configured to output a candidate set of integer ambiguities.

10. Method of claim 7, wherein the method uses carrier phase measurements of the GNSS signals and the candidate sets of integer ambiguities are processed to estimate parameters useful to determine the position.

11. Method of claim 1, wherein the first set includes the plurality of GNSS satellites from which a GNSS signal is observed by the receiver.

12. Method of claim 1, wherein the second set includes fewer than the plurality of GNSS satellites from which a GNSS signal is observed by the receiver.

27. Computer program comprising computer-readable instructions configured, when executed on a computer, to cause the computer to carry out the method according to claim 1.

13. Apparatus configured to estimate parameters derived at least from global navigational satellite system (GNSS) signals useful to determine a position, comprising:

an obtaining unit configured for obtaining at least one GNSS signal observed at a GNSS receiver from each of a plurality of GNSS satellites;

a first receiving unit configured for receiving global correction information useful to correct at least the obtained GNSS signals from a first set of GNSS satellites among the plurality of GNSS satellites, wherein the global correction information includes correction information which is independent from the position to be determined;

a second receiving unit configured for receiving local correction information useful to correct at least the obtained GNSS signals from a second set of GNSS satellites among the plurality of GNSS satellites, wherein the local correction information includes correction information which is dependent on the position to be determined;

a first processing unit configured for processing the obtained GNSS signals from the first set of GNSS satellites by using the global correction information; and

a second processing unit configured for processing the obtained GNSS signals from the second set of GNSS satellites by using the local correction information;

wherein the first set of GNSS satellites is different from the second set of GNSS satellites.

14. Apparatus of claim 13, wherein the local correction information includes at least one of

a) raw data of a single reference receiver;

b) synthetic or semi-synthetic raw data generated for a position near the position to be determined; and

c) raw data from a network of reference stations.

15. Apparatus of claim 13, wherein the second receiving unit is configured for receiving local correction information from a local source.

16. Apparatus of claim 15, wherein the local source is any one of a reference station and a reference station network.

17. Apparatus of claim 13, wherein the global correction information includes at least one of

satellite clock correction;

satellite orbit correction; and

satellite bias.

18. Apparatus of claim 13, wherein the apparatus uses carrier phase measurements of the GNSS signals.

19. Apparatus of claim 18, wherein the first processing unit is configured for processing the obtained GNSS signals from the first set of GNSS satellites by using the global correction information by:

inputting at least part of the global correction information to a geometry filter configured to output a candidate set of integer ambiguities.

20. Apparatus of claim 18, wherein the second processing unit is configured for processing the obtained GNSS signals from the second set of GNSS satellites by using the local correction information by:

inputting at least part of the local correction information to at least one ionospheric filter configured to output a candidate set of integer ambiguities.

21. Apparatus of claim 18, wherein the second processing unit is configured for processing the obtained GNSS signals from the second set of GNSS satellites by using the local correction information by:

inputting at least part of the local correction information to at least one code carrier filter configured to output a candidate set of integer ambiguities.

22. Apparatus of claim 19, wherein the apparatus uses carrier phase measurements of the GNSS signals and the candidate sets of integer ambiguities are processed to estimate parameters useful to determine the position.

23. Apparatus of claim 13, wherein the first set includes the plurality of GNSS satellites from which a GNSS signal is observed by the receiver.

24. Apparatus of claim 13, wherein the second set includes fewer than the plurality of GNSS satellites from which a GNSS signal is observed by the receiver.

25. Rover comprising an apparatus according to claim 13.

26. Network station comprising an apparatus according to claim 13.