Dynamic mapping apparatus for mobile unit acquisition and method therefor

• US 5,563,606 A
• Filed: 10/03/1994
• Issued: 10/08/1996
• Est. Priority Date: 10/03/1994
• Status: Expired due to Term

• Current Assignee: CDC Propriete Intellectuelle
• Original Assignee: Motorola, Inc. (Motorola Solutions, Inc.)
• Inventors: Wang, Theresa C. Y.
• Primary Examiner(s): Issing, Gregory C.
• Application Number:
  US08/317,064
• Time in Patent Office: 736 Days
• Field of Search: 342/352, 342/353, 342/354, 342/357, 455/12.1, 455/13.3, 455/33.1
• US Class Current: 342/354
• CPC Class Codes: H04B 7/1855 using a telephonic control signal, e.g. propagation delay variation, Doppler frequency variation, power variation, beam identification

Abstract

A called subscriber unit'"'"'s geographic location is provided by a gateway and translated to location coordinates of a global coordinate system. The gateway identifies an orbiting satellite communication station servicing the subscriber unit'"'"'s location, and sends the subscriber unit'"'"'s ID and location data to the satellite. The subscriber unit'"'"'s location data is translated to an angle and range relative to the satellite'"'"'s nadir using the satellite'"'"'s ground track data. The angle and range are mapped to an antenna beam where the subscriber unit is located using a look-up table onboard the satellite. An acquisition or ring-alert signal is transmitted within the antenna beam where the subscriber unit is located. When the range is outside the satellite'"'"'s footprint, the subscriber unit'"'"'s ID and location data are routed directly to another satellite currently servicing that location.

Claims

1. In a communication system having a gateway and non-geostationary satellite nodes, each providing a plurality of antenna beams that move with respect to earth'"'"'s surface, a method of identifying one of said antenna beams in which a subscriber unit is located comprising the steps of:

(a) determining a geographic location of said subscriber unit by said gateway, said geographic location being in earth-based coordinates;

(b) identifying a satellite node having a footprint region presently servicing said geographic location, said footprint region being defined by ground projections of said plurality of antenna beams provided by said satellite node;

(b1) sending said earth-based coordinates to said satellite node;

(b2) converting, at said satellite node, said earth-based coordinates to satellite-based coordinates, said satellite-based coordinates being relative to said identified satellite node;

(c) mapping said satellite-based coordinates to a first antenna beam provided by said satellite node; and

(d) transmitting an acquisition signal to said subscriber unit in said first antenna beam.

2. A method as claimed in claim 1 wherein said identified satellite node has said footprint region presently servicing said geographic location, and wherein each satellite node is an orbiting satellite that has movement with respect to earth'"'"'s surface.

3. A method as claimed in claim 2 wherein the identifying step includes the step of identifying said satellite node based on ground track data of said plurality of satellite nodes, said ground track data being stored in a satellite control facility that provides said ground track data to said gateway that performs the identifying step.

4. A method as claimed in claim 3 wherein:

the determining step further comprises the step of converting, at said gateway, said geographic location to said earth-based coordinates, said earth-based coordinates comprising a first and second angle relative to a vector through earth'"'"'s center identifying a unique position on earth'"'"'s surface; and

the converting step further comprises the step of translating, at said satellite node, said earth-based coordinates into said satellite-based coordinates, said satellite-based coordinates comprising a third angle and a range, said third angle and said range being relative to a nadir vector of said identified satellite node, said nadir vector passing substantially through a center point of said footprint region, and

the mapping step comprises the step of mapping said third angle and said range to said first antenna beam.

5. A method as claimed in claim 4 wherein each of said antenna beams provided by said identified satellite node have angles and ranges associated therewith relative to said nadir vector, said angles and ranges associated with each of said antenna beams being stored in said identified node, and wherein the mapping step comprises the step of mapping said third angle and said range to said first antenna beam based on said angles and ranges stored in said satellite node.

6. A method as claimed in claim 4 wherein each satellite node is an orbiting satellite that has movement with respect to earth'"'"'s surface, and wherein the mapping step comprises the step of looking up said angle and range in a look-up table stored in said satellite node, and wherein said range represents a ground range vector from said center point of said footprint region, and said third angle is between a flight path projection vector of said node and said ground range vector.

7. A method as claimed in claim 1 further comprising the step of receiving a ring-alert request at said gateway, said ring-alert request being initiated by a calling party, and wherein the determining step includes the step of determining said geographic location based on a registration of said subscriber unit in response to the receipt of said ring-alert request.

8. A method as claimed in claim 7 wherein the determining step includes the step of determining said geographic location based on a termination of a prior call by said subscriber unit.

9. A method as claimed in claim 7 wherein the sending step further comprises the step of sending a subscriber ID which uniquely identifies said subscriber unit to said identified satellite node, and wherein the transmitting step further comprises the step of transmitting said subscriber ID within said first antenna beam.

10. A method as claimed in claim 9 wherein the transmitting step further comprises the step of transmitting a ring-alert message directed to said subscriber unit in said first antenna beam, said ring-alert message including said subscriber ID.

11. A method as claimed in claim 4 further comprising the step of (e) determining by said identified satellite node, whether said range is within said footprint region of said identified satellite node.

12. A method as claimed in claim 11 further comprising the steps of:

identifying a second satellite node of said communication system having a second footprint region when step (e) determines that said range is not within said footprint region, said geographic location being within said second footprint region; and

sending said earth-based coordinates to said second satellite node.

13. A method as claimed in claim 12 further comprising the steps of:

mapping said earth-based coordinates to a second antenna beam associated with said second footprint region; and

transmitting said acquisition signal to said subscriber unit in said second antenna beam.

14. A method as claimed in claim 13 further comprising the steps of updating a nadir location of said second satellite node and sending said nadir location to a satellite control facility, the updating step being performed by a navigation processor located on said second satellite node, said nadir location being associated with a center point of said second footprint region.

15. A communication system comprising:

a communication node that provides a plurality of antenna beams, said communication being in non-geostationary orbit, said communication node having a footprint region defined by ground projections of said antenna beams; and

a gateway that comprises;

means for determining a geographic location of a subscriber unit, said geographic location being in earth-based coordinates; and

means for sending said earth-based coordinates to said communication node, said communication node having been identified as having said footprint region servicing said geographic location, and

said communication node includes means for converting said earth-based coordinates to satellite-based coordinates, said satellite-based coordinates being relevant to said communication node means for mapping said earth-based coordinates to a first antenna beam of said plurality of antenna beams provided by said satellite node; and

means for transmitting an acquisition signal to said subscriber unit in said first antenna beam.

16. A communication system as claimed in claim 15 wherein said gateway includes means for identifying said communication node from a plurality of communication nodes, wherein said communication node has said footprint region servicing said geographic location, and wherein each of said communication nodes is an orbiting satellite communication station that has movement with respect to earth'"'"'s surface.

17. A communication system as claimed in claim 16 wherein said gateway includes means for identifying said communication node based on ground track data of said communication node and said geographic location, said ground track data being stored in a satellite control facility that provides said ground track data to said gateway.

18. A communication system as claimed in claim 17 wherein:

said gateway includes means for converting said geographic location to said earth-based coordinates, said earth-based coordinates comprising a first and second angle relative to a vector through earth'"'"'s center identifying a unique position on earth'"'"'s surface; and

said communication node includes means for translating said earth-based coordinates into said satellite-based coordinates, said satellite-based coordinates comprising a third angle and a range, said third angle and said range being relative to a nadir vector of said communication node, said nadir vector passing through a center point of said footprint region, and

said means for mapping includes means for mapping said third angle and said range to said first antenna beam.

19. A communication system as claimed in claim 18 wherein each of said antenna beams has angles and ranges of said satellite-based coordinates associated therewith relative to said nadir vector, said angles and ranges associated with each of said antenna beams being stored in said communication node.

20. A communication system as claimed in claim 19 wherein said communication node has a storage means for storing said angles and ranges in a look-up table that associates said angles and ranges with one of said antenna beams, and wherein each of said ranges is a ground range vector from said center point of said footprint region, and each of said angles is between a flight path projection vector of said communication node, and said ground range vector.

21. A method of dynamically mapping location information between coordinate systems comprising the steps of:

determining a geographic location of a subscriber unit in a first coordinate system, said geographic location defined by a first and second angle relative to a vector through earth'"'"'s center;

translating said first and second angle to a second coordinate system to arrive at a third angle and a range, said third angle and said range being relative to a nadir vector of an orbiting communication station, wherein said orbiting communication station has a footprint region servicing said geographic location;

identifying an antenna beam within said footprint region based on said third angle and range; and

transmitting a signal within said antenna beam from said orbiting communication station to said subscriber unit.

22. A method as claimed in claim 21 wherein said orbiting communication station has a plurality of antenna beams associated therewith, said antenna beams being projected onto earth'"'"'s surface and defining said footprint region, said method further comprising the step of mapping said third angle and said range to said antenna beam using a look-up table stored in said orbiting communication station, said look-up table associating each antenna beam of said plurality with angles and ranges relative to said satellite'"'"'s nadir vector.