Satellite differential positioning receiver using multiple base-rover antennas

• US 9,035,826 B2
• Filed: 02/08/2012
• Issued: 05/19/2015
• Est. Priority Date: 01/30/2008
• Status: Active Grant

• Current Assignee: Javad GNSS, Inc.
• Original Assignee: Javad GNSS, Inc.
• Inventors: Ashjaee, Javad, Rapoport, Lev B., Kinkulkin, Dmitry, Yefriemov, Vladimir
• Primary Examiner(s): Phan, Dao
• Application Number:
  US13/369,227
• Publication Number:
  US 20120139784A1
• Time in Patent Office: 1,196 Days
• Field of Search: 342/357.24, 342/357.26, 342/357.27, 342/357.34, 342/357.44, 342/357.52, 701/468, 701/470
• US Class Current: 342/357.27
• CPC Class Codes: G01S 19/14 specially adapted for specific applications
• CPC Class Codes: G01S 19/44 Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method
• CPC Class Codes: G01S 19/54 using carrier phase measurements; using long or short baseline interferometry

Abstract

A rover processor determines position of a rover based upon the interaction between multiple antennas located at the rover and multiple antennas located at a base. The rover antennas may include a rover master antenna having a phase center located at the centroid of the antennas patterns of at least two auxiliary rover antennas. The rover processor may determine the position of the rover master antenna based upon the relative positions of at least two rover antennas (e.g., the rover master antenna and at least one rover auxiliary antenna, or at least two rover auxiliary antennas) with respect to at least two antennas of a base transceiver.

Claims

1. A navigation apparatus comprising:

a rover receiver including at least two rover antennas;

an orientation unit for determining orientation of the at least two rover antennas; and

rover processing logic for determining a first position of the rover receiver based upon the orientation and the position of at the least two rover antennas with respect to at least two base antennas of a base transceiver.

2. The navigation apparatus of claim 1, wherein the base transceiver includes:

at least two base antennas; and

base processing logic having access to the positions of the at least two base antennas.

3. The navigation apparatus of claim 2, wherein the positions of the at least two base antennas are referenced to an earth-centered reference frame.

4. The navigation apparatus of claim 2, wherein the base processing logic is operable to determine a positional correction of the at least two base antennas.

5. The navigation apparatus of claim 4, wherein the base transceiver is operable to transmit to the rover receiver the positional correction.

6. The navigation apparatus of claim 2, wherein the base processing logic is operable to determine an average positional correction with respect to the at least two base antennas.

7. The navigation apparatus of claim 6, wherein the base transceiver is operable to transmit to the rover receiver the average positional correction.

8. The navigation apparatus of claim 7, wherein

the rover processing logic is operable to determine a second position of the rover receiver based upon navigational signals received from navigational satellites, and to correct the second position of the rover receiver using the average positional correction.

9. The navigation apparatus of claim 2, wherein the positions of the at least two base antennas accessed by the base processing logic is derived from an orientation of the at least two base antennas provided by an orientation unit.

10. The navigation apparatus of claim 1, wherein

the base transceiver is operable to transmit to the rover receiver a redundant set of baseline measurements, and

the receiver processing logic is operable to compare a second position of the rover receiver determined from one baseline measurement of the redundant set to at least one third position of the rover receiver determined from another baseline measurement of the redundant set to thereby check for consistency.

11. The navigation apparatus of claim 10, wherein the at least two rover antennas include four rover antennas, the at least two base antennas include four base antennas, and the redundant set of baselines includes 16 baselines.

12. A computer-implemented method for determining position of a rover receiver, wherein the rover receiver includes at least two rover antennas, the method comprising:

determining orientation of the at least two rover antennas; and

determining a first position of the rover receiver based upon the orientation and the position of the at least two rover antennas with respect to at least two base antennas of a base transceiver.

13. The method of claim 12, wherein the base transceiver includes:

at least two base antennas; and

base processing logic having access to the positions of the at least two base antennas.

14. The method of claim 13, comprising determining a positional correction of the at least two base antennas.

15. The method of claim 14, comprising transmitting to the rover receiver the positional correction.

16. The method of claim 13, comprising determining an average positional correction with respect to the at least two base antennas.

17. The method of claim 16, comprising transmitting to the rover receiver the average positional correction.

18. The method of claim 17, comprising:

determining a second position of the rover receiver based upon navigational signals received from navigational satellites; and

correcting the second position of the rover receiver using the average positional correction.

19. The method of claim 13, wherein the positions of the at least two base antennas accessed by the base processing logic are derived from an orientation of the at least two base antennas provided by an orientation unit.

20. The method of claim 12, comprising:

transmitting to the rover receiver a redundant set of baseline measurements, and

comparing a second position of the rover receiver determined from one baseline measurement of the redundant set to at least one third position of the rover receiver determined from another baseline measurement of the redundant set to thereby check for consistency.

21. A non-transitory computer readable medium comprising computer-executable instructions for determining position of a rover receiver, wherein the rover receiver includes at least two rover antennas, the instructions for:

determining orientation of the at least two rover antennas; and

determining a first position of the rover receiver based upon the orientation and the position of the at least two rover antennas with respect to at least two base antennas of a base transceiver.

22. The non-transitory computer-readable medium of claim 21, wherein the base transceiver includes:

at least two base antennas; and

base processing logic having access to the positions of the at least two base antennas.

23. The non-transitory computer-readable medium of claim 22, comprising instructions for determining a positional correction of the at least two base antennas.

24. The non-transitory computer-readable medium of claim 23, comprising instructions for transmitting to the rover receiver the positional correction.

25. The non-transitory computer-readable medium of claim 22, comprising instructions for determining an average positional correction with respect to the at least two base antennas.

26. The non-transitory computer-readable medium of claim 25, comprising instructions for transmitting to the rover receiver the average positional correction.

27. The non-transitory computer-readable medium of claim 26, comprising instructions for:

determining a second position of the rover receiver based upon navigational signals received from navigational satellites; and

correcting the second position of the rover receiver using the average positional correction.

28. The non-transitory computer-readable medium of claim 22, wherein the positions of the at least two base antennas accessed by the base processing logic are derived from an orientation of the at least two base antennas provided by an orientation unit.

29. The non-transitory computer-readable medium of claim 21, comprising instructions for:

transmitting to the rover receiver a redundant set of baseline measurements, and comparing a second position of the rover receiver determined from one baseline measurement of the redundant set to at least one third position of the rover receiver determined from another baseline measurement of the redundant set to thereby check for consistency.