Direct geolocation from TDOA, FDOA and AGL

• US 9,625,566 B2
• Filed: 05/21/2014
• Issued: 04/18/2017
• Est. Priority Date: 05/21/2014
• Status: Active Grant

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: Raytheon Company (Rtx Corporation)
• Inventors: Broad, John T.
• Primary Examiner(s): Adams, Tashiana
• Assistant Examiner(s): SERAYDARYAN, HELENA H
• Application Number:
  US14/283,826
• Publication Number:
  US 20160299212A1
• Time in Patent Office: 1,063 Days
• Field of Search: 342465
• CPC Class Codes: G01S 5/04 Position of source determined by a plurality of spaced direction-finders
• CPC Class Codes: G01S 5/12 by co-ordinating position lines of different shape, e.g. hyperbolic, circular, elliptical or radial

Abstract

A direct geolocation approach for estimating a location of a stationary emitter located on the Earth surface is provided. The approach uses data collected during a plurality of time periods including Time Difference of Arrival (TDOA) and Frequency Difference of Arrival (FDOA) measurements of a radar pulse sent from the emitter, and altitude measurements of an aircraft above the Earth surface. The approach includes estimating a location of the emitter for each of the time periods based on the TDOA, FDOA, and altitude measurements associated with a respective time period. The estimated location of the stationary emitter includes possible longitude and latitude of the emitter. The approach further includes averaging the estimated locations associated with the plurality of time periods to form an averaged estimated location of the emitter. A convenient example of the approach computes the location of the emitter based on the averaged estimated location.

Claims

1. A method for estimating a location of a stationary emitter located on the Earth surface, the method comprising:

collecting data during a plurality of time periods, the data including Time Difference of Arrival (TDOA) and Frequency Difference of Arrival (FDOA) measurements of a radar pulse sent from a stationary emitter located on the Earth surface and received by at least two antennas on an aircraft, and altitude measurements of the aircraft above the Earth surface;

for each of the plurality of time periods, estimating a location of the stationary emitter based on the TDOA, FDOA, and altitude measurements associated with a respective time period, the result being an estimated location of the stationary emitter associated with the respective time period, the estimated location of the stationary emitter including a candidate longitude and a candidate latitude of the stationary emitter;

averaging the estimated locations associated with the plurality of time periods forming an averaged estimated location of the stationary emitter, the averaged estimated location including an average of the candidate longitudes and an average of the candidate latitudes of the stationary emitter; and

providing the averaged estimated location of the stationary emitter,

wherein estimating includes calculating two solutions for each of the estimated locations,

wherein averaging includes maintaining a first averaged estimated location and a second averaged estimated location, each being a running average of the solutions calculated for the estimated locations, and associating each of the solutions with either the first or second averaged estimated location based on proximity of each of the solutions to either the first or second averaged estimated location, and

wherein providing includes selecting either the first or second averaged estimated location having a range to the aircraft closest in value to a computed range from the aircraft to the stationary emitter.

2. The method of claim 1 wherein estimating includes representing each of the TDOA, FDOA, and altitude measurements as a surface in three dimensional space;

identifying an intersection of the surfaces; and

based on the identification, returning each identified intersection as one of the estimated location of the stationary emitter.

3. The method of claim 2 wherein each of the surfaces is described by a simultaneous equation;

and

wherein identifying includes solving the simultaneous equations using Laguerre'"'"'s method.

4. The method of claim 1 wherein calculating the solutions includes identifying solutions that are consistent with locations on the Earth surface as valid solutions;

and

wherein associating includes including the valid solutions in the first and second averaged estimated locations.

5. The method of claim 1 wherein associating includes for each solution, determining whether a respective solution is closer in proximity to either the first or second averaged estimated location;

and

based on the determination, including the respective solution in the running average of either the first or second averaged estimated location.

6. The method of claim 5 further comprising determining the computed range from a ratio of effective radiated power of the stationary emitter to received power of the stationary emitter.

7. The method of claim 1 wherein averaging includes assigning weights to each of the estimated locations based on an approximation of noise in the data collected during the plurality of time periods;

and

averaging the estimated locations according to the assigned weights resulting in a weighted-average estimated location of the stationary emitter.

8. The method of claim 1 wherein providing includes providing the averaged estimated location of the stationary emitter to a user.

9. The method of claim 1 further comprising computing a location of the stationary emitter on the Earth surface based on the averaged estimated location of the stationary emitter being provided.

10. A system for estimating a location of a stationary emitter located on the Earth surface, the system comprising:

a memory having computer executable instructions thereupon;

at least one interface receiving Time Difference of Arrival (TDOA) and Frequency Difference of Arrival (FDOA) measurements of a radar pulse sent from a stationary emitter located on the Earth surface and received by at least two antennas on an aircraft, and receiving an altitude measurement of the aircraft above the Earth surface;

an estimating engine coupled to the memory and the at least one interface, the computer executable instructions when executed by the estimating engine cause the estimating engine to;

for each of the plurality of time periods, estimate a location of the stationary emitter based on the TDOA, FDOA, and altitude measurements associated with a respective time period, the result being an estimated location of the stationary emitter associated with the respective time period, the estimated location of the stationary emitter including a candidate longitude and a candidate latitude of the stationary emitter;

average the estimated locations associated with the plurality of time periods forming an averaged estimated location of the stationary emitter, the averaged estimated location including an average of the candidate longitudes and an average of the candidate latitudes of the stationary emitter; and

provide the averaged estimated location of the stationary emitter,

wherein estimating includes calculating two solutions for each of the estimated locations,

wherein averaging includes maintaining a first averaged estimated location and a second averaged estimated location, each being a running average of the solutions calculated for the estimated locations, and associating each of the solutions with either the first or second averaged estimated location based on proximity of each of the solutions to either the first or second averaged estimated location, and

wherein providing includes selecting either the first or second averaged estimated location having a range to the aircraft closest in value to a computed range from the aircraft to the stationary emitter.

12. The method of claim 10 wherein calculating the solutions includes identifying solutions that are consistent with locations on the Earth surface as valid solutions;

and

wherein associating includes including the valid solutions in the first and second averaged estimated locations.

13. The system of claim 10 wherein associating includes for each solution, determining whether a respective solution is closer in proximity to either the first or second averaged estimated location;

and

based on the determination, including the respective solution in the running average of either the first or second averaged estimated location.

14. The system of claim 13 wherein the computed range is determined from a ratio of effective radiated power of the stationary emitter to received power of the stationary emitter.

11. A tangible non-transitory computer-readable storage medium having computer readable instructions stored therein for estimating a location of a stationary emitter located on the Earth surface, which when executed by one or more processors cause the one or more processors, given data collected during a plurality of time periods including Time Difference of Arrival (TDOA) and Frequency Difference of Arrival (FDOA) measurements of a radar pulse sent from a stationary emitter located on the Earth surface and received by at least two antennas on an aircraft, and an altitude measurement of the aircraft above the Earth surface, to:

for each of the plurality of time periods, estimate a location of the stationary emitter based on the TDOA, FDOA, and altitude measurements associated with a respective time period, the result being an estimated location of the stationary emitter associated with the respective time period, the estimated location of the stationary emitter including a candidate longitude and a candidate latitude of the stationary emitter;

average the estimated locations associated with the plurality of time periods forming an averaged estimated location of the stationary emitter, the averaged estimated location including an average of the candidate longitudes and an average of the candidate latitudes of the stationary emitter; and

provide the averaged estimated location of the stationary emitter,

wherein estimating includes calculating two solutions for each of the estimated locations,

wherein averaging includes maintaining a first averaged estimated location and a second averaged estimated location, each being a running average of the solutions calculated for the estimated locations, and associating each of the solutions with either the first or second averaged estimated location based on proximity of each of the solutions to either the first or second averaged estimated location, and

wherein providing includes selecting either the first or second averaged estimated location having a range to the aircraft closest in value to a computed range from the aircraft to the stationary emitter.

15. The tangible non-transitory computer-readable storage medium of claim 11 further comprising computer readable instructions stored therein wherein calculating the solutions includes identifying solutions that are consistent with locations on the Earth surface as valid solutions;

and

wherein associating includes including the valid solutions in the first and second averaged estimated locations.

16. The tangible non-transitory computer-readable storage medium of claim 11 further comprising computer readable instructions stored therein wherein associating includes for each solution, determining whether a respective solution is closer in proximity to either the first or second averaged estimated location;

and

based on the determination, including the respective solution in the running average of either the first or second averaged estimated location.

17. The tangible non-transitory computer-readable storage medium of claim 16 further comprising computer readable instructions stored therein wherein the computed range is determined from a ratio of effective radiated power of the stationary emitter to received power of the stationary emitter.