Vessel attitude determination system and method

• US 5,933,110 A
• Filed: 07/13/1998
• Issued: 08/03/1999
• Est. Priority Date: 07/13/1998
• Status: Expired due to Term

• Current Assignee: ARINC Incorporated (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: ARINC Incorporated (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Howell, Eugene B., English, Donald W., Tang, Wang
• Primary Examiner(s): Tarcza, Thomas
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US09/114,298
• Time in Patent Office: 386 Days
• Field of Search: 342/352, 342/357, 701/213, 701/215
• US Class Current: 342/357.37
• CPC Class Codes: G01S 19/55 Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method

Abstract

A portable attitude determination apparatus and method are disclosed that can be used with a ship docking system. At least two receivers on a vessel receive Global Positioning System (GPS) satellite data. GPS carrier phase measurements are used to determine attitude (i.e., roll, pitch and yaw angles) of a moving platform. The phase measurements are processed to determine a precise vector from one receiver phase center to the other. The azimuth and elevation of a baseline vector is then computed. Float ambiguities between the two receivers are determined, and are used to provide initial estimates of antenna baseline length and attitude. A search procedure is then employed to find the actual integer ambiguities. Only GPS observables are needed; no other external data input is required.

Claims

1. An apparatus for determining an attitude, comprising:

a pair of GPS antennas capable of receiving GPS carrier signals from a plurality of GPS satellites; and

a processor that determines the attitude based upon floating point ambiguities between said GPS carrier signals received by each of said pair of GPS antennas.

2. The apparatus of claim 1, wherein said processor determines said attitude by filtering the double difference floating point ambiguities from phase and psuedorange measurements taken by the pair of GPS antennas based on the GPS carrier signals.

3. The apparatus of claim 1, wherein said processor determines said attitude by calculating an antenna baseline length based on the floating point ambiguities and the phase measurements taken by the pair of GPS antennas based on the GPS carrier signals.

4. The apparatus of claim 1, wherein said processor determines said attitude by estimating initial azimuth and elevation values that are based upon said floating point ambiguities.

5. The apparatus of claim 4, wherein said processor determines said attitude by searching through a range of azimuth and elevation values, wherein the size of each of the ranges are based upon the accuracy of said initial azimuth and elevation values.

6. The apparatus of claim 5, wherein said processor determines said attitude by determining integer ambiguities based upon said search through said ranges of azimuth and elevation values.

7. The apparatus of claim 1, wherein said processor determines said attitude by permitting said floating point ambiguities to converge during a settling period.

8. The apparatus of claim 7, wherein said processor determines said attitude by conducting a 3-dimensional search through azimuth, elevation and baseline length values based upon said converged floating point ambiguities to establish initial estimates for azimuth, elevation and baseline length values.

9. The apparatus of claim 8, wherein said processor determines said attitude by conducting a second 3-dimensional search through azimuth, elevation and baseline length values to resolve integer ambiguities.

10. The apparatus of claim 9, wherein said processor determines said attitude by conducting said second search by computing the minimum of a cost function based on phase measurements taken by said pair of GPS antennas based upon said GPS carrier signals.

11. The apparatus of claim 1, wherein said baseline length is predetermined and said processor determines said attitude based on said floating point ambiguities and phase measurements taken by said pair of GPS antennas based upon said GPS carrier signals and said predetermined baseline length.

12. The apparatus of claim 11, wherein said processor determines said attitude by conducting a 2-dimensional search through azimuth and elevation values based upon said floating point ambiguities after said floating point ambiguities have converged during a settling period.

13. The apparatus of claim 12, wherein said processor determines said attitude by conducting a 2-dimensional search through azimuth and elevation values using initial estimates of azimuth and elevation from an external source.

14. The apparatus of claim 12, wherein said processor determines said attitude by conducting a 2-dimensional search in a search window whose size is based on the accuracy of initial estimates of azimuth and elevation values that are used for the search and which are based upon said floating point ambiguities.

15. The apparatus of claim 12, wherein said processor determines said attitude by conducting said 2-dimensional search by computing the minimum of a cost function based on phase measurements taken by said pair of GPS antennas based on said GPS carrier signals.

16. A method for determining an attitude, comprising:

receiving GPS carrier signals from a plurality of GPS satellites at a pair of GPS antennas; and

determining the attitude based upon floating point ambiguities between said GPS carrier signals received by each of said pair of GPS antennas.

17. The method of claim 16, wherein said determining comprises filtering the double difference floating point ambiguities from phase and pseudorange measurements taken by said pair of GPS antennas based on said GPS carrier signals.

18. The method of claim 16, wherein said determining comprises determining an antenna baseline length based on said floating point ambiguities and on phase measurements of said GPS carrier signals.

19. The method of claim 16, wherein said determining comprises estimating initial azimuth and elevation values that are based on said floating point ambiguities.

20. The method of claim 19, wherein said determining further comprises searching through a range of azimuth elevation values, wherein the size of each of said ranges is based upon the accuracy of said initial azimuth and elevation values.

21. The method of claim 20, wherein said determining further comprises determining integer ambiguities during said search.

22. The method of claim 16, wherein said determining comprises permitting said floating point ambiguities to converge during a settling period.

23. The method of claim 22, wherein said determining further comprises conducting a 3-dimensional search through azimuth, elevation and baseline length values based on said converged floating point ambiguities to establish initial estimates for azimuth, elevation and baseline length values.

24. The method of claim 23, wherein said determining further comprises conducting a second 3-dimensional search through azimuth, elevation and baseline length values to resolve integer ambiguities.

25. The method of claim 24, wherein said conducting said second 3-dimensional search comprises determining the minimum of a cost function based on phase measurements of said GPS carrier signals.

26. The method of claim 16, wherein said determining is further based on phase measurements of said GPS carrier signals and on a predetermined baseline length.

27. The method of claim 16, wherein said determining comprises conducting a 2-dimensional search through azimuth and elevation values after said floating point ambiguities have converged during a settling period.

28. The method of claim 27, wherein said searching is conducted using initial azimuth and elevation values from a source external to said pair of GPS antennas.

29. The method of claim 27, wherein said search is conducted in a search window whose size is based on the accuracy of initial estimates of azimuth and elevation values used for said search and which are based upon said floating point ambiguities.

30. The method of claim 27, wherein said conducting said 2-dimensional search comprises determining the minimum of a cost function based on phase measurements of said GPS carrier signals.