Ambiguity resolution for ambiguous position solutions using satellite beams

• US 5,920,284 A
• Filed: 09/30/1996
• Issued: 07/06/1999
• Est. Priority Date: 09/30/1996
• Status: Expired due to Term

• Current Assignee: Qualcomm, Inc.
• Original Assignee: Qualcomm, Inc.
• Inventors: Victor, Edward B.
• Primary Examiner(s): Tarcza, Thomas
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US08/723,723
• Time in Patent Office: 1,009 Days
• Field of Search: 342/357, 342/457, 455/12.1, 455/13.1, 701/213
• US Class Current: 342/357.64
• CPC Class Codes: G01S 1/04 Details
• CPC Class Codes: G01S 19/01 Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
• CPC Class Codes: G01S 5/0036 of measured values, i.e. measurement on mobile and position calculation on base station

Abstract

A system and method for resolving ambiguity in an ambiguous position solution for a user terminal position in a satellite communications system which includes a user terminal, at least one satellite, and a gateway communicating with the user terminal through the satellite. Each satellite has a plurality of satellite beams which each illuminate a region on the Earth in a known pattern relative to a satellite sub-track. A satellite beam illuminating the user terminal is identified along with its corresponding position relative to the sub-track. The orientations of possible user terminal positions and the identified beam relative to the satellite sub-track are compared to each other. Possible user terminal positions falling on an incorrect side of the sub-track from the detected beam illuminating the user terminal, are considered as incorrect solutions for that user terminal. The ambiguity solution can be determined using satellite identification and comparison elements in the user terminal, or at the gateway, in which case certain beam information is reported to the gateway. In further aspects of the invention, the beam being identified can be either a forward link or reverse link beam, or both, and each link has a different beam pattern.

Claims

1. Apparatus for resolving ambiguity in position determinations for a satellite communications system, comprising:

a user terminal;

at least one satellite having a first plurality of satellite beams for forward link communications and a second plurality of beams for reverse link communications each communicating with a region of the Earth'"'"'s surface in a known pattern relative to a satellite sub-track, the beam pattern of each plurality differing from that of the other;

a gateway communicating with said user terminal through said at least one satellite using at least one of said first and second plurality of satellite beams, and being configured for determining a plurality of possible positions of said user terminal on the Earth'"'"'s surface;

first identification means for identifying a first satellite beam communicating with said user terminal on said forward link and a corresponding side of said sub-track said first beam is on;

second identification means for identifying a second satellite beam communicating with said user terminal on said reverse link and a corresponding side of said sub-track said second beam is on; and

comparison means for comparing said plurality of possible positions with said corresponding sub-track sides for said first and second identified satellite beams to select one of said plurality of possible positions based on the result of said comparison.

2. The ambiguity resolution apparatus of claim 1 further comprising:

first identification means in said user terminal for detecting at least one beam specific parameter for said first satellite beam illuminating said user terminal;

transfer means in said user terminal for reporting a value for said beam specific parameter to said gateway; and

reception means in said gateway for receiving said value and for identifying said first satellite beam illuminating said user terminal based on said reported value; and

second identification means in said gateway for identifying said second satellite beam used by said user terminal on said reverse link to communicate with said gateway.

3. The ambiguity resolution apparatus of claim 2 wherein said one beam specific parameter comprises a PN code phase.

4. The ambiguity resolution apparatus of claim 1, further comprising means for determining a plurality of possible positions of said user terminal on the Earth'"'"'s surface.

5. The ambiguity resolution apparatus of claim 4, wherein said means for determining comprises:

parameter determining means for determining a plurality of parameters describing the geometric relationships between said user terminal and said at least one satellite; and

position determining means for determining said plurality of possible positions based on said plurality of parameters and said position and velocity of said at least one satellite.

6. The ambiguity resolution apparatus of claim 5, wherein said parameter determining means comprises range parameter determining means for determining a range parameter.

7. The ambiguity resolution apparatus of claim 5, wherein said parameter determining means comprises range-rate parameter determining means for determining a range-rate parameter.

8. A position determining system for a satellite communications system, comprising:

a user terminal;

at least one satellite having a first plurality of satellite beams for forward link communications and a second plurality of beams for reverse link communications, each satellite beam communicating with a region of the Earth'"'"'s surface in a known pattern relative to a satellite sub-track, the beam pattern of each plurality differing from that of the other;

a gateway communicating with said user terminal through said at least one satellite using at least one of said first and second plurality of satellite beams;

range parameter determining means for determining a range parameter;

range-rate parameter determining means for determining a range-rate parameter;

position determining means in said gateway for determining a plurality of possible positions of said user terminal on the Earth'"'"'s surface based on said range parameter, said range-rate parameter, and position and velocity of said at least one satellite;

first identification means for identifying a first satellite beam illuminating said user terminal on said forward link and a corresponding side of said sub-track said first beam is on;

second identification means for identifying a second satellite beam communicating with said user terminal on said reverse link and a corresponding side of said sub-track said second beam is on; and

comparison means for comparing said plurality of possible positions with said corresponding sub-track sides for said first and second identified satellite beams to select one of said plurality of possible positions based on the result of said comparison.

9. In a communications system comprising a user terminal, at least one satellite, and a gateway for communicating with the user terminal through the satellite and determining a plurality of possible positions of the user terminal on the Earth'"'"'s surface, each satellite having a first plurality of satellite beams for forward link communications and a second plurality of beams for reverse link communications each communicating with a region of the Earth'"'"'s surface in a known pattern relative to a satellite sub-track, the beam pattern of each plurality differing from that of the other, a method for resolving ambiguity in the position of the user terminal on the Earth'"'"'s surface, comprising the steps of:

identifying a first beam of said first plurality of satellite beams which is illuminating the user terminal on said forward link and a first corresponding side of a satellite sub-track said first beam is positioned on;

identifying a second beam of said second plurality of satellite beams which is communicating with said user terminal on said reverse link and a second corresponding side of a satellite sub-track said second beam is positioned on; and

comparing the plurality of possible positions with the said determined first and second sub-track sides for said identified satellite beams to select one of the plurality of possible positions based on the result of said comparison.

10. The ambiguity resolution method of claim 9 further comprising the steps of:

detecting at least one beam specific parameter for the satellite first beam communicating with said user terminal on said forward link;

reporting a value for said beam specific parameter from said user terminal to said gateway; and

receiving said value in said gateway and identifying said first satellite beam illuminating said user terminal based on said reported value.

11. The ambiguity resolution method of claim 10 wherein said step of detecting one beam specific parameter comprises detecting a phase of a received PN code.

12. The ambiguity resolution method of claim 9, further comprising the step of determining the plurality of possible positions of the user terminal on the Earth'"'"'s surface.

13. The system of claim 12, wherein said determining step comprises the steps of:

determining a plurality of parameters describing the geometric relationships between the user terminal and the at least one satellite; and

determining the plurality of possible positions based on said plurality of parameters and the position and velocity of the at least one satellite.

14. The method of claim 13, wherein said plurality of parameters includes a range parameter.

15. The method of claim 13, wherein said plurality of parameters includes a range-rate parameter.