Method and system for terrain aided navigation

• US 6,512,976 B1
• Filed: 04/27/2001
• Issued: 01/28/2003
• Est. Priority Date: 04/27/2001
• Status: Expired due to Term

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Martinez, Steven D., Cox, Paul A., Sabatino, Anthony E., Romero, Leroy G., Pyne, Michael D.
• Primary Examiner(s): LOUIS JACQUES, JACQUES H
• Application Number:
  US09/844,912
• Time in Patent Office: 641 Days
• Field of Search: 701/200, 701/207, 701/208, 701/213, 342/456, 342/357.02, 342/357.08, 342/357.01, 342/26, 342/29, 342/179, 342/63, 342/64, 342/46, 342/42, 342/43, 702/94, 340/961, 340/963, 340/968, 340/970
• US Class Current: 701/207
• CPC Class Codes: G01C 21/005 with correlation of navigation data from several sources, e.g. map or contour matching G01C21/30 takes precedence
• CPC Class Codes: G01S 13/86 Combinations of radar systems with non-radar systems, e.g. sonar, direction finder

Abstract

A method and system for terrain aided navigation which provide more precise and more accurate position, velocity, altitude, and attitude for an air vehicle. The present method is a continuous, active, all-weather, day/night, self-contained vehicle system used for terminal and en route navigation. The present method utilizes on-vehicle sensing elements which require no external stimulation, eliminating dependence on external ground and space-based navigation aides. The present method also provides a drift-free solution. The present method is more difficult to detect (sense) and more difficult to disrupt.

Claims

1. A method for terrain aided navigation, the method comprising the steps of:

a) providing a first vehicle state estimation from a navigational computation source;

b) correlating data from a RADAR sensor with terrain data from an on board source to provide a second vehicle state estimation;

c) integrating the first vehicle state estimation with the second vehicle state estimation; and

d) outputting an enhanced vehicle state estimation from the navigational computation source.

2. The method of claim 1 wherein the step of correlating data from a RADAR sensor with terrain data comprises broadcasting a low probability of detection RADAR signal.

3. The method of claim 2 wherein the step of broadcasting a low probability of detection RADAR signal comprises broadcasting a narrow RADAR signal.

4. The method of claim 2 wherein the step of broadcasting a low probability of detection RADAR signal comprises broadcasting a short duration of transmission RADAR signal.

5. The method of claim 2 wherein the step of broadcasting a low probability of detection RADAR signal comprises broadcasting a low power RADAR signal.

6. The method of claim 2 wherein the step of broadcasting a low probability of detection RADAR signal comprises broadcasting a spread spectrum emission RADAR signal.

7. The method of claim 2 wherein the step of broadcasting a low probability of detection RADAR signal comprises broadcasting a frequency hopping RADAR emission signal.

8. The method of claim 2 wherein the step of broadcasting a low probability of detection RADAR signal comprises broadcasting a directed RADAR signal.

9. The method of claim 1 further comprising the step of providing a day/night sensor.

10. The method of claim 1 further comprising the step of providing an all weather sensor.

11. The method of claim 1 wherein the step of correlating data from a RADAR sensor with terrain data comprises measuring a bearing and a range to an object above the terrain.

12. The method of claim 11 wherein the step of measuring a bearing and a range to an object above the terrain comprises computing an altitude of the object above a datum.

13. The method of claim 11 wherein the step of measuring the bearing and range to an object comprises using more than one RADAR sensor.

14. The method of claim 13 wherein the step of using more than one RADAR sensor comprises using one transmitter and more than one receiver.

15. The method of claim 14 wherein the step of using one transmitter and more than one receiver comprises using an interferometer.

16. The method of claim 1 wherein the step of correlating comprises measuring a bearing and range to at least one object with the RADAR sensor and comparing with the on-board terrain data and the first vehicle state estimation.

17. The method of claim 16 wherein the at least one object comprises an object at a highest elevation.

18. The method of claim 1 wherein the step of providing a first vehicle state estimation from a navigational computation source comprises providing a member from the group consisting of satellite based navigation, inertial navigation, ground based navigation, doppler navigation and dead reckoning navigation.

19. The method of claim 1 further comprising continuously repeating steps a) through d).

20. A system for terrain aided navigation comprising:

a RADAR sensor;

an on-board source for providing terrain data;

a navigation computation source comprising a first vehicle state estimation;

a means for correlating data from the RADAR sensor with the terrain data to provide a second vehicle state estimation;

a means for integrating the first vehicle estimation with the second vehicle state estimation; and

an output from the navigation computation source comprising an enhanced vehicle state estimation.

21. The invention of claim 20 wherein said RADAR sensor comprises a low probability of detection RADAR signal.

22. The invention of claim 21 wherein said RADAR sensor comprises a narrow RADAR signal.

23. The invention of claim 21 wherein said RADAR sensor comprises a short duration of transmission RADAR signal.

24. The invention of claim 21 wherein said RADAR sensor comprises a low power RADAR signal.

25. The invention of claim 21 wherein said RADAR sensor comprises a spread spectrum emission RADAR signal.

26. The invention of claim 21 wherein said RADAR sensor comprises a frequency hopping RADAR emission signal.

27. The invention of claim 21 wherein said RADAR sensor comprises a directed RADAR signal.

28. The invention of claim 20 wherein said RADAR sensor comprises a day/night sensor.

29. The invention of claim 20 wherein said RADAR sensor comprises an all weather sensor.

30. The invention of claim 20 wherein said means for correlating data comprises a means for measuring a bearing and a range to an object above the terrain.

31. The invention of claim 30 wherein said means for measuring a bearing and a range to an object above the terrain comprises an apparatus for computing an altitude of the object above a datum.

32. The invention of claim 30 wherein said means for measuring a bearing and a range to an object above the terrain comprises more than one RADAR sensor.

33. The invention of claims 32 wherein said more than one RADAR sensor comprises one transmitter and more than one receiver.

34. The invention of claim 33 wherein said one transmitter and more than one receiver comprises an interferometer.

35. The invention of claim 20 wherein said correlated data comprises a bearing and range to at least one object from said RADAR sensor and comparing with on-board terrain data and the first vehicle state estimation output.

36. The invention of claim 35 wherein said at least one object comprises and object at a highest elevation.

37. The invention of claim 20 wherein said first vehicle state estimation comprises a member from the group consisting of satellite based navigation, inertial navigation, ground based navigation, doppler navigation and dead reckoning navigation.