US6087974A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Monopulse system for target location
Assignee: Lockheed Martin Corp
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Filing: 1998-08-03
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Granted: 2000-07-11
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Expires: 2018-08-03
Abstract
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.
Inventors
- 👤 Kai-Bor Yu
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 01:30
CPC Classifications
F; F41; F41G; F41G7/00; F41G7/20; F41G7/22; F41G7/2246; F41G7/2226; F41G7/2273; F41G7/2286; G; G01; G01S; G01S13/00; G01S13/02; G01S13/06; G01S13/42; G01S13/44; G01S13/4409; G01S13/4427; G01S13/4463
Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
103 words
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.
Claim 2
Independent Claim
103 words
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.
Claim 3
Dependent Claim
49 words
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.
Claim 4
Dependent Claim
59 words
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.
Claim 5
Dependent Claim
64 words
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.
Claim 6
Dependent Claim
26 words
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.
Claim 7
Dependent Claim
56 words
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.
Claim 8
Independent Claim
141 words
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.
Claim 9
Independent Claim
141 words
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.
Claim 10
Independent Claim
78 words
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.
Claim 11
Independent Claim
78 words
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.
Claim 12
Dependent Claim
76 words
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.
References Cited (Backward Citations)
US5382954A
Cited
US5371506A
Cited
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| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
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