Integrated navigation and communication satellite system

• US 5,841,398 A
• Filed: 11/20/1996
• Issued: 11/24/1998
• Est. Priority Date: 11/20/1996
• Status: Expired due to Term

• Current Assignee: Space Systems/Loral Incorporated (Loral Space and Communications Incorporated)
• Original Assignee: Space Systems/Loral Incorporated (Loral Space and Communications Incorporated)
• Inventors: Brock, J. Kurt
• Primary Examiner(s): FELBER, JOSEPH LEON
• Application Number:
  US08/753,111
• Time in Patent Office: 734 Days
• Field of Search: 342/357, 701/215
• US Class Current: 342/357.395
• CPC Class Codes: G01S 19/115 Airborne or satellite based pseudolites or repeaters

Abstract

A system and method for improving the accuracy of pseudorange error measurements at a receiving or user station by utilizing a communications satellite as an additional ranging source for providing navigational signal information, wherein the user station, in fixing its position on the Earth, receives a pseudorange signal directly from a GPS satellite and also a pseudorange indicative or pseudorange-error indicative signal from a communications satellite which re-broadcasts, a time tagged, indicative signal to serve as another observable in pseudorange equations computed in the user station. The communications satellite may receive a pseudorange signal directly, or an error indicative signal from an Earth-based station, for conversion into the pseudorange indicative or error indicative signal it transmits. A particular embodiment for incorporation in a communications satellite constellation, such as Globalstar™, involves a reference station, or network of reference stations disposed at appropriate Earth locations, for providing pseudorange error signals from their locations that are collected at a masterstation in a satellite gateway for processing and then transmitting by the gateway to a communications satellite. The satellite converts and re-transmits the processed information to a user station at another Earth location where the received information is used, along with directly received GPS information signals, to enhance the navigational position accuracy of the user station. Thus, an additional ranging source is provided that improves the accuracy, availability, and integrity of the pseudorange measurements.

Claims

1. A satellite system for integrating navigation and communications information, comprising:

navigational satellite means for providing navigational reference signals;

communications satellite means for receiving transmitted communications signals and re-transmitting communications signals indicative thereof;

transmitting means, in said communications satellite means, for transmitting signals indicative of said navigational reference signals; and

receiver station means for receiving communications signals re-transmitted from said communications satellite means, and comprising;

means, receiving navigational reference signals directly from said navigational satellite means and said indicative navigational reference signals from said transmitting means in said communications satellite means, for performing calculations using both of said reference signals to provide enhanced position and time information for said receiver station means; and

wherein said transmitting means comprises;

means for receiving navigational reference signals directly from said navigational satellite means; and

means for converting said navigational reference signals to indicative navigational reference signals for transmitting to said receiver station means.

2. A system as in claim 1, further comprising:

antenna means for transmitting navigational error indicative signals to said communications satellite means;

at least one reference station for receiving navigational reference signals directly from said navigational satellite means, and using said navigational reference signals to provide pseudorange error signals to said antenna means for transmitting as said navigational error indicative signals; and

wherein said transmitting means further comprises;

means for receiving said navigational error indicative signals from said antenna means; and

means for converting said navigational error indicative signals to indicative navigational reference signals for transmitting to said receiver station means.

3. A system as in claim 1 further comprising:

Earth-based station means for transmitting navigational error indicative signals to said communications satellite means;

processing means for providing said navigational error indicative signals to said Earth-based station means;

a plurality of Earth-fixed reference stations for receiving navigational reference signals directly from said navigational satellite means, each of said reference stations comprising;

means for using said navigational reference signals to provide pseudorange error signals; and

means for transmitting said pseudorange error signals to said processing means for collection and conversion to navigational error indicative signals provided to said Earth-based station means for transmitting to said communication satellite means; and

wherein said transmitting means further comprises;

means for receiving said navigational error indicative signals from said Earth-based station means; and

means for converting said navigational error indicative signals to indicative navigational reference signals for transmitting to said receiver station means.

4. A system as in claim 3 wherein said processing means comprises a master station and said Earth-based station means comprises a satellite gateway antenna.

5. A system as in claim 1 wherein said indicative navigational reference signals comprise pseudorange signals and said means for performing calculations comprises means for using said pseudorange signals in pseudorange equations to evaluate position and time for said receiver station means.

6. A system as in claim 1 wherein said indicative navigational reference signals comprise pseudorange error signals and said means for performing calculations comprises means for using said pseudorange error signals in pseudorange equations to evaluate position and time for said receiver station means.

7. A system as in claim 1 wherein said navigational satellite means comprises a plurality of GPS satellites and said communications satellite means comprises an LEO satellite.

8. A system as in claim 1 wherein said means for performing calculations comprises interface card means for formatting said indicative navigational reference signals for use in performing said calculations to provide enhanced position and time information for said receiver station means.

9. A method for integrating satellite navigation and communications information, comprising the steps of:

locating at least one navigational satellite that produces navigational reference signals;

locating at least one communications satellite that receives transmitted communications signals and re-transmits signals indicative thereof;

relaying, from said communications satellite, signals indicative of said navigational reference signals;

receiving at a receiver station, that receives indicative communications signals from said communications satellite, navigational reference signals directly from said navigational satellite and said indicative navigational reference signals relayed from said communications satellite; and

performing appropriate calculations using both of said reference signals to provide enhanced position and time information for said receiver station; and

wherein said relaying step comprises;

receiving navigational reference signals at said communications satellite directly from said navigational satellite; and

converting said navigational reference signals to said indicative navigational reference signals for transmitting to said receiver station.

10. The method of claim 9 wherein said navigational reference signals are pseudorange signals and said step of performing appropriate calculations comprises evaluating pseudorange equations.

11. The method of claim 9 wherein said relaying step further comprises:

receiving navigational reference signals in the form of pseudorange signals at said communications satellite directly from said navigational satellite; and

processing said pseudorange signals into pseudorange error signals and converting said pseudorange error signals to said indicative navigational reference signals for transmitting to said receiver station.

12. The method of claim 9, comprising the further steps of:

receiving navigational reference signals directly from said navigational satellite means at an Earth-based reference station and using said navigational reference signals to produce pseudorange error signals;

processing said pseudorange error signals into navigational error indicative signals;

transmitting said navigational error indicative signals to said communications satellite; and

receiving said navigational error indicative signals in said communications satellite and converting said navigational error indicative signals to indicative navigational reference signals for relaying to said receiver station.

13. The method of claim 9 comprising the further steps of:

disposing a plurality of Earth-fixed reference stations for receiving navigational reference signals directly from said navigational satellite and using said navigational reference signals to provide respective pseudorange error signals;

collecting said pseudorange error signals and converting them to navigational error indicative signals;

transmitting said navigational error indicative signals to said communications satellite; and

receiving said navigational error indicative signals in the communications satellite and converting said navigational error indicative signals to indicative navigational reference signals for relaying to said receiver station.

14. The method of claim 9 wherein said indicative navigational reference signals comprise pseudorange signals and said step of performing appropriate calculations comprises using said pseudorange signals in pseudorange equations to evaluate position and time for said receiver station.

15. The method of claim 9 wherein said indicative navigational reference signals comprise pseudorange error signals and said step of performing appropriate calculations comprises using said pseudorange error signals in pseudorange equations to evaluate position and time for said receiver station.