Satellite position fixing

• US 6,219,615 B1
• Filed: 03/26/1998
• Issued: 04/17/2001
• Est. Priority Date: 04/01/1997
• Status: Expired due to Fees

• Current Assignee: ICO Services, Ltd. (Dish Network Corporation)
• Original Assignee: ICO Services, Ltd. (Dish Network Corporation)
• Inventors: Chambers, Charles
• Primary Examiner(s): Cuchlinski, Jr., William A.
• Assistant Examiner(s): ARTHUR JEANGLAUDE, GERTRUDE
• Application Number:
  US09/048,062
• Time in Patent Office: 1,118 Days
• Field of Search: 701/207, 701/213, 701/214, 701/215, 701/216, 701/300, 342/357.01, 342/357.02, 342/357.08, 455/12.1
• US Class Current: 701/213
• CPC Class Codes: G01S 19/38 Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
• CPC Class Codes: G01S 5/0289 of multiple transceivers, e.g. in ad hoc networks
• CPC Class Codes: H04B 7/1855 using a telephonic control signal, e.g. propagation delay variation, Doppler frequency variation, power variation, beam identification

Abstract

In a satellite position fixing system, where an earth station 38 communicates with a satellite 10 which, in turn, communicates with selectable ones out of a plurality of user terminals 44 whose position, on the surface of the earth 14, is measured, the accuracy of measurement of the position of the satellite 10 is improved by using all of the user terminals 44 as further triangulation points, the improved position being incorporated in further user terminal 44 position determinations, and so on to create a cumulative improvement. Weighting is applied so that user terminals 44 with large errors in triangulation are given small significance and those with small errors are given great significance.

Claims

1. A system for estimating a position of a satellite of a mobile communication system at a particular instant of time wherein said satellite is operable to cooperate with an earth station to measure and record the position of a terminal on the surface of the earth by reference to an estimated, instant position of said satellite, said earth station being operable to estimate said instant position of said satellite with a first accuracy, wherein said system is operable to incorporate the measured position of said terminal to make a re-estimation of said instant position of said satellite with a second accuracy, said second accuracy being greater than said first accuracy.

2. A system according to claim 1 operable to employ the result of said re-estimation as the new estimated instant position of said satellite when next operable to measure the position of said terminal.

3. A system according to claim 1 wherein said terminal is one of a plurality of terminals, and wherein said system is operable to measure and record the position of each of said plurality of terminals and to incorporate the measured position of each of said plurality of terminals to execute said re-estimation in each instance.

4. A system according to claim 3 wherein said plurality of terminals can incorporate one or more other earth stations.

5. A system according to claim 1 operable, in said re-estimation, to incorporate a weighting to the significance of the accuracy and geometry of the measurement of the position of said terminal, and to employ said weighting to give greater favour to those measurements of position of said terminal which contribute most to improving the accuracy of estimation of the instant position of said satellite.

6. A system according to claim 5 wherein said weighting is incorporated in said re-estimation by providing said accuracy of measurement and said geometry as state variable inputs to a Kalman filter algorithm.

7. A system according to claim 1 wherein said earth station is one of a plurality of earth stations, each of said plurality of earth stations sharing information concerning said re-estimation.

8. A method for estimating a position of a satellite of a mobile communication system at a particular instant of time for use in a system wherein said satellite is operable to cooperate with an earth station to measure and record the position of a terminal on the surface of the earth by reference to an estimated, instant position of said satellite, said earth station being operative to estimated said instant position of said satellite with a first accuracy, said method including the step of incorporating the measured position of said terminal in a re-estimation of said instant position of said satellite with a second accuracy, said second accuracy being greater than said first accuracy.

9. A method according to claim 8 including the step of employing the result of said re-estimation as the new estimated instant position of said satellite when next said system is operable to measure the position of said terminal.

10. A method according to claim 8 wherein said terminal is one of a plurality of terminals, and including the steps of measuring and recording the position of each of said plurality of terminals and incorporating the measured position of each of said plurality of terminals and executing said re-estimation in each instance.

11. A method according to claim 10 including the step of including, in said plurality of terminals, one or more other earth stations.

12. A method according to claim 8 including the steps of including, in said re-estimation, a weighting to the significance of the accuracy and geometry of the measurement of the position of said terminal, and employing said weighting to give greater favour to those measurements of position of said terminal which contribute most to improving the accuracy of estimation of the instant position of said satellite.

13. A method according to claim 12 including the step of including said weighting is in said re-estimation by providing said accuracy of measurement and said geometry as state variable inputs to a Kalman filter algorithm.

14. A method, according to claim 8 wherein said earth station is one of a plurality of earth stations, and including the step of each of said plurality of earth stations sharing information concerning said re-estimation.