Matrix monopulse ratio radar processor for two target azimuth and elevation angle determination

• US 6,404,379 B1
• Filed: 06/29/2000
• Issued: 06/11/2002
• Est. Priority Date: 06/29/2000
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Zheng, Yibin, Yu, Kai-Bor
• Primary Examiner(s): Sotomayor, John B.
• Application Number:
  US09/607,004
• Time in Patent Office: 712 Days
• Field of Search: 342/80, 342/147, 342/148, 342/149, 342/152, 342/194, 342/195
• US Class Current: 342/80
• CPC Class Codes: G01S 13/44 Monopulse radar, i.e. simultaneous lobing
• CPC Class Codes: G01S 13/4418 with means for eliminating radar-dependent errors in angle measurements, e.g. multipath effects

Abstract

A method and system for identifying the locations of plural targets lying within a main beam of a monopulse antenna including four ports for generating sum, elevation difference, azimuth difference and double difference signals. The method comprises the steps of forming a monopulse ratio matrix from the sum, elevation difference, azimuth difference and double difference signals; and determining eigenvalues of the monopulse ratio matrix. These eigenvalues are then used to determine the angular locations of the plural targets. Preferably, the eigenvalues are determined by performing an eigenvalue decomposition of the monopulse ratio matrix to generate eigenvalues, and the angles of the targets may be determined from the eigenvalues by the use of a look-up table.

Claims

1. A method for identifying the locations of plural targets lying within a main beam of a monopulse antenna including at least four ports for generating sum, elevation difference, azimuth difference and double difference signals, the method comprising the steps of:

forming a monopulse ratio matrix from the sum, elevation difference, azimuth difference and double difference signals;

determining eigenvalues of the monopulse ratio matrix; and

using the eigenvalues to determine the angular locations of the plural targets.

2. A method according to claim 1, wherein the determining step includes the step of performing an eigenvalue decomposition of the monopulse ratio matrix to generate eigenvalues.

3. A method according to claim 1, wherein:

the forming step includes the steps of

i) forming a monopulse ratio azimuth matrix, and

ii) forming a monopulse ratio elevation matrix;

the determining step includes the steps of

i) determining an eigenvalue decomposition of the monopulse ratio azimuth matrix, and

ii) determining an eigenvalue decomposition of the monopulse ratio elevation matrix; and

the using step includes the steps of

i) using the eigenvalues of the monopulse ratio azimuth matrix to determine azimuth angles of the targets, and

ii) using the eigenvalues of the monopulse ratio elevation matrix to determine elevation angles of the targets.

4. A method according to claim 3, wherein the step of using the eigenvalues include the step of determining a pairing of azimuth and elevation angles of the targets based on the similarity of the eigenvectors of the monopulse ratio azimuth and elevation matrices.

5. A method according to claim 1, wherein the step of using the eigenvalues includes the step of using the eigenvalues to obtain angles of the targets from a look-up table.

6. A system for identifying the locations of plural targets lying within a main beam of a monopulse antenna including four ports for generating sum, elevation difference, azimuth difference and double difference signals, the method comprising the steps of:

means for forming a monopulse ratio matrix from the sum, elevation difference, azimuth difference and double difference signals;

means for determining the eigenvalue decomposition of the monopulse ratio matrix; and

means for using the eigenvectors to determine the angular locations of the plural targets.

7. A system according to claim 6, wherein the determining means includes the means for performing an eigenvalue decomposition of the monopulse ratio matrix to generate eigenvalues.

8. A system according to claim 6, wherein:

the forming means includes

i) means for forming a monopulse ratio azimuth matrix, and

ii) means for forming a monopulse ratio elevation matrix;

the determining means includes

i) means for determining an eigenvalue decomposition of the monopulse ratio azimuth matrix, and

ii) means for determining an eigenvalue decomposition of the monopulse ratio elevation matrix; and

the using means includes

i) means for using the eigenvalues of the monopulse ratio azimuth matrix to determine azimuth angles of the targets, and

ii) means for using the eigenvalues of the monopulse ratio elevation matrix to determine elevation angles of the targets.

9. A system according to claim 8, wherein the using means include the means for determining a pairing of azimuth and elevation angles of the targets based on the similarity of the eigenvectors of the monopulse ratio azimuth and elevation matrices.

10. A system according to claim 6, wherein the using means includes means for using the eigenvalues to obtain angles of the targets from a look-up table.

11. A method for processing information in a main beam of a monopulse antenna including four ports for generating sum, elevation difference, azimuth difference and double difference signals, the method comprising the steps of:

forming a set of monopulse ratios from the sum, elevation difference, azimuth difference and double difference signals; and

comparing said ratios to determine whether there is one target or two targets lying within the main beam.

12. A method according to claim 11, further comprising the step of, if there one target lying within the main beam, averaging formed ratios to determine azimuth and elevation angles for said one target.

13. A method according to claim 11, further comprising the step of, if there are two targets lying within the main beam, further processing the sum, elevation difference, azimuth difference, and double difference signal to determine azimuth and elevation angles for each of the targets.