IP Library Granted Patent US 8,791,859
Granted Patent B2
US 8,791,859 · App. 13/298,260 · Granted Jul 29, 2014

High precision radio frequency direction finding system

Inventor: Clayton J. Larson (Acton, CA)
Assignee: Lockheed Martin Corporation
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Quick Facts
Patent No.
US 8,791,859
App. No.
13/298,260
Granted
Jul 29, 2014
Kind
B2
Abstract

High precision radio frequency direction finding systems are described that can determine an angle-of-arrival and geo-location of a RF emitter with respect to a mobile platform. A radio frequency direction finding (RFDF) system for determining a position of a RF emitter with respect to a mobile platform can include an angle-of-azimuth (AoA) system configured to determine an azimuth of a RF emitter with respect to the mobile platform; an attitude measurement system configured to measure the attitude of the mobile platform; a geo-location system configured to calculate the geo-location of the RF emitter; and a processor system configured to calculate a position of the RF emitter.

Claims (31)

1. A radio frequency direction finding (RFDF) system for determining a position of a RF emitter with respect to a mobile platform, the system comprising:

an angle-of-azimuth (AoA) system configured to determine an azimuth of a RF emitter with respect to the mobile platform, wherein the AoA system comprises a RF interferometer;

an attitude measurement system configured to measure the attitude of the mobile platform;

a geo-location system configured to calculate the geo-location of the RF emitter;

a processor system configured to calculate a position of the RF emitter; and

an alignment system configured to align the RF interferometer.

2. The RFDF system of claim 1 , wherein the RF interferometer comprises an antenna array having a plurality of antennas.

3. The RFDF system of claim 2 , wherein the RF interferometer comprises a plurality of receivers, each connected to one of the plurality of antennas.

4. The RFDF system of claim 2 , wherein the RF interferometer comprises a plurality of phase comparators, each connected to one of the plurality of receivers.

5. The RFDF system of claim 3 , wherein each of the plurality of phase comparators is connected to a unique pair of the plurality of receivers.

6. The RFDF system of claim 2 , wherein the interferometer comprises a processor configured to implement the multiple signal classification (MUSIC) algorithm as an interferometry algorithm.

7. The RFDF system of claim 1 , wherein the attitude measurement system comprises a differential global position system (GPS) for determining the attitude of the mobile platform.

8. The RFDF system of claim 7 , wherein the differential GPS system is configured to determine the geo-location of the mobile platform.

9. The RFDF system of claim 1 , further comprising a database of topological data.

10. The RFDF system of claim 1 , further comprising a memory location including topological data.

11. The RFDF system of claim 1 , wherein the attitude measurement system comprises an inertial navigation system for determining the attitude of the mobile platform.

12. The RFDF system of claim 1 , further comprising one or more GPS receivers.

13. The RFDF system of claim 1 , wherein the alignment system comprises a built-in-test (BIT) system configured to align the RF interferometer.

14. The RFDF system of claim 1 , wherein the alignment system is configured to provide test waveforms to the RF interferometer.

15. The RFDF system of claim 1 , wherein the AoA system is configured to determine azimuth of the RF emitter utilizing phase measurements.

16. The RFDF system of claim 15 , wherein the AoA system is further configured to determine azimuth of the RF emitter utilizing amplitude measurements.

17. A radio frequency direction finding (RFDF) system for determining a position of a RF emitter with respect to a mobile platform, the system comprising:

an interferometer including an antenna array configured to determine an azimuth of a RF emitter with respect to the mobile platform, wherein the antenna array is configured for implementation on the mobile platform;

an attitude measurement system configured to measure the attitude of the mobile platform;

a geo-location system configured to calculate the geo-location of the RF emitter;

a geo-location system configured to calculate the geo-location of the mobile platform;

a processor system configured to calculate a position of the RF emitter with respect to the mobile platform; and

an alignment system configured to align the interferometer.

18. The RFDF system of claim 17 , wherein the interferometer comprises a processor configured to implement the multiple signal classification (MUSIC) algorithm as an interferometry algorithm.

19. The RFDF system of claim 17 , wherein the attitude measurement system comprises an inertial navigation system for determining the attitude of the mobile platform.

20. The RFDF system of claim 17 , wherein the attitude measurement system comprises a differential GPS system.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 18, 2011
From: LARSON, CLAYTON J.
To: LOCKHEED MARTIN CORPORATION
Reel/Frame 027264/0779 →
Continuity (1)
Related Publication 20130120192A1 · May 16, 2013