Tactical all weather precision guidance and navigation system

• US 20060071849A1
• Filed: 09/30/2004
• Published: 04/06/2006
• Est. Priority Date: 09/30/2004
• Status: Abandoned Application

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Kim, Paul Y., Weinman, Glonn J., Howle, William M., Wheeler, Stanloy L., Holden, Chad, Knecht, George W.
• Application Number:
  US10/953,274
• Publication Number:
  US 20060071849A1
• Time in Patent Office: Days
• US Class Current: 342/357.310
• CPC Class Codes: G01S 19/071 DGPS corrections
• CPC Class Codes: G01S 19/18 Military applications

Abstract

Precision navigation within a theater of operations is performed by receiving, at each of a plurality of spaced apart known locations, GPS satellite signals from a plurality of GPS satellites, wherein the known locations approximately define the theater of operations. A measure of error in the GPS satellite signal for each of the plurality of GPS satellites is determined. The measures of error in the GPS satellite signals are utilized to correct GPS satellite signals received at an unknown location within the theater of operations. The corrected GPS satellite signals are then used to determine a precise position of the unknown location within the theater of operations.

Claims

1. A system for precise relative navigation, comprising:

a plurality of reference sensors that receive data from the global positioning system;

a central processing node that receives global positioning system satellite data from each of the reference sensors, computes a set of correction parameters for each satellite based upon error detecting and minimizing algorithms housed in the central processing node, and transmits said correction parameters; and

a weapon system that receives data from the global positioning system, receives the correction parameters from the central processing node, and generates from the received data and the received correction parameters precise position information and steers itself to a target in accordance with the precise position information.

2. A method for precision navigation within a theater of operations, comprising:

receiving via GPS receivers, at each of a plurality of spaced apart known locations, GPS satellite signals from a plurality of GPS satellites, wherein the known locations approximately define the theater of operations;

providing the received GPS satellite signals to a central processing node;

filtering the provided signals to differentiate between errors local to the known locations and errors specific to the GPS satellites;

determining GPS satellite clock and ephemeris corrections based on the differentiated errors; and

transmitting the determined GPS satellite clock and ephemeris corrections to mobile units within the theater of operations.

3. The method of claim 2, wherein the determined corrections are transmitted indirectly to the mobile units.

4. The method of claim 2, wherein the received GPS satellite signals are provided asynchronously to the central processing node.

5. The method of claim 2, comprising:

prior to filtering, replacing tropospheric delay corrections added at the spaced apart known locations to the received GPS satellite signals with tropospheric delay corrections that are based on weather data for the known locations.

6. The method of claim 5, wherein the replacement tropospheric delay corrections are derived from a Black &

Eisner tropospheric delay model.

7. The method of claim 2, wherein the filtering is performed utilizing an Extended Kalman Filter.

8. The method of claim 7, wherein the Extended Kalman Filter includes states for clock errors of the GPS receivers at the plurality of spaced apart known locations;

and

9. The method of claim 8, wherein the Extended Kalman Filter includes line-of-sight bias residual states for each GPS satellite at each of the plurality of spaced apart known locations.

10. The method of claim 2, comprising transmitting local weather data to mobile units within the theater of operations.

11. The method of claim 10, comprising:

a first mobile unit transmitting information about its own location to the central processing unit; and

the central processing unit transmitting weather data to the first mobile unit, wherein the transmitted weather data corresponds to a location of the first mobile unit.

12. The method of claim 2, comprising:

the central processing unit receiving information from a mobile unit wherein the information indicates the mobile unit'"'"'s location;

the central processing unit determining an ionospheric correction corresponding to the mobile unit'"'"'s location, based on the received GPS satellite signals; and

transmitting the determined ionospheric correction to the mobile unit.

13. The method of claim 12, wherein the determined correction is transmitted indirectly to the mobile unit.

14. The method of claim 2, wherein after the central processing unit receives an new Issue of Data Ephemeris;

the central processing unit continues to utilize the previous Issue of Data Ephemeris and corresponding corrections until corrections for the new Issue of Data Ephemeris are available.

15. A system for precision navigation and guidance within a theater of operations, comprising:

a plurality of spaced apart GPS sensors at calibrated locations that approximately define the theater of operations;

means for determining a measure of error in GPS satellite signals received by each GPS sensor; and

means for using the measures of error in GPS satellite signals to correct GPS satellite signals received at an unknown location within the theater of operations; and

means for using the corrected GPS satellite signals to precisely locate the unknown location within the theater of operations.

16. The system of claim 15, wherein:

each of the GPS sensors is selected from a group consisting of stationary and mobile GPS sensors.

17. The system of claim 15, wherein the GPS sensors are spaced one from another up to a maximum separation such that the GPS sensors have line of sight communications with at least four common GPS satellites.

18. The system of claim 15, further including:

means with a mobile platform within the theater of operations for receiving the measure of error in GPS satellite signals and using the measure of error to correct GPS signals received at the mobile platform; and

means at the mobile platform for using the corrected GPS signals to determine a precise location of the mobile platform.

19. The system of claim 15, further including:

means with a fire control platform within the theater of operations for receiving the measure of error in GPS satellite signals and using the measure of error to correct GPS signals received at the fire control platform; and

means at the fire control platform for using the corrected GPS signals to determine a precise location of the fire control platform.

20. The system of claim 15, further including:

means with a weapon deployed within the theater of operations for receiving the measure of error in GPS satellite signals and using the measure of error in GPS satellite signals to precisely guide the weapon to a target location within the theater of operations.

21. A method of precisely determining a location within a theater of operations that is approximately defined by a plurality of spaced apart known locations, the method comprising:

at each of the plurality of spaced apart known locations, receiving geolocation satellite signals from a plurality of geolocation satellites, wherein;

the geolocation satellite signals include time information; and

for any one of the geolocation satellites, the time information included in the geolocation satellite signals received at one of the spaced apart locations is not the same as the time information included in the geolocation satellite signals received at another of the spaced apart locations;

communicating the received geolocation satellite signals from the known locations to a processing node;

the processing node reordering the communicated geolocation satellite signals according to the time information included in the communicated geolocation satellite signals;

for each of the geolocation satellites, using the reordered geolocation satellite signals and information about the known locations to estimate an error in the received geolocation satellite signals;

for each of the geolocation satellites, communicating the estimated error to a position-determining device within the theater of operations;

the position-determining device receiving geolocation satellite signals from the geolocation satellites;

the position-determining device using the estimated errors to correct each of the received geolocation satellite signals; and

the position-determining device using the corrected geolocation satellite signals to precisely determine the location of the position-determining device within the theater of operations.

22. The method of claim 21, wherein for each of the geolocation satellites, using the reordered geolocation satellite signals and information about the known locations to estimate the error in the received geolocation satellite signals comprises using a Kalman filter to estimate the error in the received geolocation satellites.

23. The method of claim 22, wherein the Kalman filter includes a state representing an orbital position of the geolocation satellite.

24. The method of claim 22, wherein the Kalman filter includes a state representing a clock phase of the geolocation satellite.

25. The method of claim 22, wherein the Kalman filter includes states representing a clock phase at each of the spaced apart known locations.

26. The method of claim 22, wherein the Kalman filter includes states representing a clock frequency at each of the spaced apart known locations.

27. The method of claim 21, wherein communicating the received geolocation satellite signals from the known locations to the processing node includes communicating by means of Ethernet technology.

28. The method of claim 21, wherein communicating the received geolocation satellite signals from the known locations to the processing node includes communicating by means of the Internet.

29. The method of claim 21, wherein communicating the received geolocation satellite signals from the known locations to the processing node includes communicating by means of dedicated telephone connections.

30. The method of claim 21, wherein communicating the received geolocation satellite signals from the known locations to the processing node includes communicating by means of a satellite communication system.