Monopulse system for target location

• US 6,087,974 A
• Filed: 08/03/1998
• Issued: 07/11/2000
• Est. Priority Date: 08/03/1998
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Yu, Kai-Bor
• Primary Examiner(s): Gregory, Bernarr E.
• Application Number:
  US09/128,282
• Time in Patent Office: 708 Days
• Field of Search: 342/61, 342/62, 342/67, 342/73, 342/74, 342/80, 342/147, 342/149, 342/150, 342/151, 342/152, 342/153, 342/154, 342/175, 342/195, 342/378, 342/379, 342/380, 342/381, 342/382 , 342/383, 342/384, 342/385, 342/417, 342/422, 342/427, 342/29, 342/75, 342/13, 342/14, 342/15, 342/16, 342/17, 342/18, 342/19, 342/20, 244/3.1, 244/13.15, 244/3.19
• US Class Current: 342/62
• CPC Class Codes: F41G 7/2226 comparing the observed data with stored target data, e.g. target configuration data
• CPC Class Codes: F41G 7/2246 Active homing systems, i.e. comprising both a transmitter and a receiver
• CPC Class Codes: F41G 7/2286 using radio waves
• CPC Class Codes: G01S 13/44 Monopulse radar, i.e. simultaneous lobing
• CPC Class Codes: G01S 13/4409 HF sub-systems particularly adapted therefor, e.g. circuits for signal combination multi-lobing aerials or aerial systems H01Q25/00
• CPC Class Codes: G01S 13/4427 with means for eliminating the target-dependent errors in angle measurements, e.g. glint, scintillation effects
• CPC Class Codes: G01S 13/4463 using phased arrays

Abstract

A monopulse system generates sum (Σ), elevation difference (Δ_EL), azimuth difference (Δ_AZ), and double difference (Δ.sub.Δ) signals, and generates a covariance matrix. The covariance matrix is decomposed to produce at least the principal eigenvector. The location or angular direction within the main beam of a single target is determined from the real component of the quotient of elements of the principal eigenvector, by the use of a look-up table. In another embodiment of the invention, the eigenvalues are generated from the covariance matrix, and the number of significant eigenvalues determines the number of targets within the main beam. If a single target is found, its location is found as described above. If two targets are found in the main beam, the locations of the two targets are determined by a closed-form solution of quadratic equations. A missile using a monopulse radar according to an aspect of the invention determines the presence of two targets within the main beam, which targets may be a real target and a decoy, and uses extrinsic information to identify a selected target as being the true target. The missile is homed in the direction of the selected target.

Claims

1. A method for identifying the locations of plural targets lying within the main beam of a monopulse antenna which includes four ports, namely sum, elevation difference, azimuth difference, and double difference ports, said method comprising the steps of:

generating a covariance matrix from the sum, elevation difference, azimuth difference, and double difference signals;

determining the number of targets within the main beam based on the eigenvalues of said covariance matrix;

if the number of targets is two, determining, from a system of two-dimensional equations derived from noise eigenvectors of said covariance matrix, the angular locations of said two targets within said main beam.

2. A method according to claim 1, wherein said step of determining the number of targets within said main beam based on the eigenvalue of the covariance matrix includes the steps of:

performing an eigenvalue decomposition of the covariance matrix to generate eigenvalues; and

determining the number of significant eigenvalues.

3. A method according to claim 2, wherein said step of determining the number of significant eigenvalues includes the step of comparing the magnitudes of said eigenvalues determined in said decomposition step with a threshold value, and deeming the number of those of said eigenvalues which have a magnitude which exceeds said threshold value to indicate said number of targets.

4. A method according to claim 1, wherein said step of determining, from a system of two-dimensional equations derived from noise eigenvectors of the covariance matrix, the angular locations of said two targets within said main beam comprises the steps of:

solving said two-dimensional polynomial derived from noise eigenvectors of the covariance matrix for azimuth and elevation components of angular location within said main beam.

5. A method according to claim 4, further comprising the step of generating said two-dimensional polynomial by the steps of:

generating said eigenvectors from said covariance matrix.

6. A method according to claim 1, further comprising the step of recurrently repeating said steps of

generating a covariance matrix;

determining the number of targets within said main beam based on eigenvalues of said covariance matrix; and

if the number of targets is two, determining the angular locations of said two targets within said main beam.

7. A method for controlling a missile for causing it to home on a target which is generating spoofing signals which are radiated within a main beam of a monopulse antenna of said missile, which monopulse antenna includes four ports, namely sum, elevation difference, azimuth difference, and double difference ports, said method comprising the steps of:

generating a covariance matrix of said sum, elevation difference, azimuth difference, and double difference signals;

determining the number of targets within said main beam based on the eigenvalues of said covariance matrix;

if the number of targets is two, determining, from a system of two-dimensional equations derived from noise eigenvectors of said covariance matrix, the angular locations of said two targets within said main beam.

from other information, identifying one of said two targets as the selected target; and

homing said missile toward said selected target.

8. A method for identifying the location or angular direction of a single target within the main beam of a monopulse antenna, said method comprising the steps of:

generating sum, elevation difference, azimuth difference, and double difference signals from the signals of said monopulse antenna;

generating a covariance matrix of said sum, elevation difference, azimuth difference, and double difference signals;

determining the direction of said single target by use of at least the principal eigenvector of said covariance matrix.

9. A method according to claim 8, wherein said step of determining the direction of said single target includes the steps of:

taking the quotient of first and second elements of said principal eigenvector, to thereby produce a first quotient;

taking the quotient of first and third elements of said principal eigenvector, to thereby produce a second quotient; and

deeming the real parts of said first and second quotients to be the angles of said single target.