System and method for determining geo location of a target using locus of emitter positions (LEP)

• US 9,383,429 B2
• Filed: 10/17/2012
• Issued: 07/05/2016
• Est. Priority Date: 10/17/2012
• Status: Active Grant

• Current Assignee: Raytheon Applied Signal Technology Incorporated (Rtx Corporation)
• Original Assignee: Raytheon Applied Signal Technology Incorporated (Rtx Corporation)
• Inventors: May, William
• Primary Examiner(s): McGue, Frank J
• Application Number:
  US13/654,155
• Publication Number:
  US 20140104112A1
• Time in Patent Office: 1,357 Days
• Field of Search: 342/450
• US Class Current: 1/1
• CPC Class Codes: G01S 11/04 using angle measurements
• CPC Class Codes: G01S 5/0242 Determining the position of transmitters to be subsequently used in positioning G01S5/0289 takes precedence
• CPC Class Codes: G01S 5/12 by co-ordinating position lines of different shape, e.g. hyperbolic, circular, elliptical or radial

Abstract

A system and method for determining geo position of a target by an aircraft, including: (a). electronically receiving navigation data related to the aircraft and multilateration information related to the target; (b). electronically calculating a locus of emitter positions (LEP) curve from the received navigation data and multilateration information; (c). repeating steps (a) and (b), as the aircraft moves toward or away from the target; (d). electronically accumulating, in a computer storage medium, the calculated LEP curves; and (e). electronically determining a position that is closest to all the accumulated LEP curves to establish a position of the target.

Claims

1. A method for determining geo position of a target by a geo-location engine onboard a moving aircraft, the geo-location engine including one or more processors, a receiver, and storage medium, the method comprising:

receiving, by the receiver, navigation data of the moving aircraft including flight attitude of the moving aircraft, and an angle to the target, via an input signal;

calculating, by the one or more processors, a locus of emitter positions (LEP) curve from the received navigation data, the flight attitude and the angle to the target, using a cone angle in a 3-D coordinate system and a single measurement of the flight attitude;

repeating, by the one or more processors, steps (a) and (b), as the moving aircraft moves toward or away from the target;

accumulating by the one or more processors, in the storage medium, the calculated LEP curves;

determining, by the one or more processors, a position that is closest to all the accumulated LEP curves to establish a position of the target, wherein the position of the target is established regardless of the distance of the moving aircraft to the target, and regardless of aircraft position relative to the target; and

transmitting the established position of the target to a navigation system.

2. The method of claim 1, wherein calculating the LEP curve further comprises converting, by the one or more processors, the received angle to a three-dimensional geometric model using the received navigation data;

and electronically intersecting the three-dimensional geometric model with a three-dimensional geometric model of the earth to obtain the LEP curve.

3. The method of claim 2, wherein the angle comprises angle of arrival (AOA) information and the three-dimensional geometric model is a three-dimensional cone model.

4. The method of claim 2, wherein the three-dimensional geometric model of the earth is a sphere.

5. The method of claim 2, wherein the three-dimensional geometric model of the earth is an ellipsoid.

6. The method of claim 2, wherein the three-dimensional geometric model of the earth is determined using digital terrain data.

7. The method of claim 1, wherein the navigation data includes position, heading, pitch and roll data.

8. The method of claim 3, wherein the AOA is measured relative to the longitudinal axis of the aircraft.

9. The method of claim 8, wherein the AOA corresponds to an azimuth, and the cone is formed by sweeping through all elevation angles.

10. The method of claim 9, wherein an apex of the cone is the aircraft, and a central axis of the cone is a reference axis used for measuring AOA.

11. A system for determining geo position of a target by a moving aircraft comprising:

a receiver for receiving navigation data related to the moving aircraft including flight attitude of the moving aircraft, and an angle to the target;

one or more processors for calculating a locus of emitter positions (LEP) curve from the received navigation data, the flight attitude and the angle to the target, using a cone angle in a 3-D coordinate system and a single measurement of the flight attitude, wherein as the moving aircraft moves toward or away from the target, the receiver receives new navigation data and new angle to the target and said one or more processors calculate new LEP curves;

a memory for accumulating the calculated LEP curves, wherein said one or more processors determine a position that is closest to all the accumulated LEP curves to establish a position of the target, and wherein the position of the target is established by said one or more processors regardless of the distance of the moving aircraft to the target, and regardless of aircraft position relative to the target; and

an output logic circuit for transmitting the established position of the target to a navigation system.

12. The system of claim 11, wherein said one or more processors are configured to calculate the LEP curve by converting the received angle to a three-dimensional geometric model using the received navigation data;

and intersecting the three-dimensional geometric model with a three-dimensional geometric model of the earth to obtain the LEP curve.

13. The system of claim 12, wherein the angle comprises angle of arrival (AOA) information and the three-dimensional geometric model is a three-dimensional cone model.

14. The system of claim 12, wherein the three-dimensional geometric model of the earth is a sphere.

15. The system of claim 12, wherein the three-dimensional geometric model of the earth is an ellipsoid.

16. The system of claim 12, wherein the three-dimensional geometric model of the earth is determined using digital terrain data.

17. The system of claim 11, wherein the navigation data includes position, heading, pitch and roll data.

18. The system of claim 13, wherein the AOA is measured relative to the longitudinal axis of the aircraft.

19. A method for determining geo position of a target by a geo-location engine onboard a moving aircraft, the geo-location engine including one or more processors, a receiver, and storage medium, the method comprising:

receiving, by the receiver, navigation data of the moving aircraft including flight attitude of the moving aircraft, and an angle to the target, via an input signal;

calculating, by the one or more processors, a locus of emitter positions (LEP) curve from the received navigation data, the flight attitude and the angle to the target, using a cone angle in a 3-D coordinate system and a single measurement of the flight attitude;

repeating, by the one or more processors, steps (a) and (b), as the moving aircraft moves toward or away from the target;

accumulating by the one or more processors, in the storage medium, the calculated LEP curves;

determining, by the one or more processors, a position that is closest to all the accumulated LEP curves to establish a position of the target, wherein the position of the target is established regardless of the distance of the moving aircraft to the target, and regardless of aircraft position relative to the target; and

transmitting the established position of the target to a target acquisition system.