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US4292634A Expired / Lapsed US ⏱️ 0.0 years remaining

Real-time multiple-look synthetic aperture radar processor for spacecraft applications

Assignee: National Aeronautics and Space Administration
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Filing: 1978-12-15
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Granted: 1981-09-29
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Expires: 1998-12-15
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Abstract

Abstract A spaceborne synthetic aperture radar having pipeline multiple-look data processing makes use of excessive azimuth bandwidth in radar echo signals to produce multiple-look images. Time multiplexed single-look image lines from an azimuth correlator go through an energy analyzer which analyzes the mean energy in each separate look to determine the radar antenna electric boresight for use in generating the correct reference functions for the production of high quality SAR images. The multiplexed single look image lines also go through a registration delay to produce multiple-look images.

Inventors

  • 👤 with respect to an invention of Frosch Robert A. Administrator of the National Aeronautics and Space Administration
  • 👤 Chialin Wu
  • 👤 Vance C. Tyree

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 22:05
CPC Classifications
G; G01; G01S; G01S13/00; G01S13/88; G01S13/89; G01S13/90; G01S13/9021; G01S13/9027

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 71 words
In a synthetic aperture data processor having pipeline multiple-look data capability with time-multiplexed single-look image lines from an azimuth correlator, the combination comprising means for analyzing the mean energy in an even number of multiple looks of the same target and means responsive to the mean energy for closed-loop control processing of delay control and reference function coefficients for said azimuth correlator to track and refine the radar antenna boresight information.
Claim 2
Dependent Claim 71 words
In a synthetic aperture data processor having pipeline multiple-look data capability with time-multiplexed single-look image lines from an azimuth correlator, the combination comprising means for analyzing the mean energy in an even number of multiple looks of the same target and means responsive to the mean energy for closed-loop control processing of delay control and reference function coefficients for said azimuth correlator to track and refine the radar antenna boresight information.
Claim 3
Dependent Claim 151 words
The combination of claim 1 werein said energy analyzing means includes means for summing the energy for each different look, means for adding the energy of the first half of the even number of multiple looks to form a first multiple look sum, means for adding the energy of the second half of the even number of multiple looks to form a second multiple look sum, means for separately forming the sum and difference of said first and second multiple look sum, and means for forming the quotient of the difference of said first and second multiple look sum divided by the sum of said first and second multiple look sum, thereby to determine a quantity M that is a measure of the symmetry of the energy on the looks relative to the center of the processing band for use in the generation of said delay control and reference function coefficients.
Claim 4
Dependent Claim 23 words
The combination of claim 2 including means connected to said correlator for registration delay of time-multiplexed single-look image lines to produce multiple-look images.
Claim 5
Dependent Claim 208 words
In a spacecraft synthetic aperture radar processor having multiple-look data capability and using an even number of time-multiplexed single-look image lines from an azimuth correlator to analyze the mean energy in each of N separate looks of the same target area to determine a quantity M which is a measure that indicates the symmetry of the energy on the looks relative to the center of the processing band for use in generating the correct delay control for range migration correction and reference functions for the production of synthetic aperture radar images, said energy analyzer comprising means for adding the single-look image lines of the first half of the even number of multiple looks and for separately adding and subtracting from the sum of the first half of the even number of multiple looks the sum of the last half of the even number of multiple looks, and from the sum and difference thus formed, producing a normalized quantity M by means for dividing the difference thus formed by the sum thus formed, and means responsive to said normalized quantity M for generating delay control and reference functions for said azimuth correlator, whereby excessive azimuth bandwidth in radar echo signals is used to produce high quality spacecraft SAR images.
Claim 6
Dependent Claim 208 words
In a spacecraft synthetic aperture radar processor having multiple-look data capability and using an even number of time-multiplexed single-look image lines from an azimuth correlator to analyze the mean energy in each of N separate looks of the same target area to determine a quantity M which is a measure that indicates the symmetry of the energy on the looks relative to the center of the processing band for use in generating the correct delay control for range migration correction and reference functions for the production of synthetic aperture radar images, said energy analyzer comprising means for adding the single-look image lines of the first half of the even number of multiple looks and for separately adding and subtracting from the sum of the first half of the even number of multiple looks the sum of the last half of the even number of multiple looks, and from the sum and difference thus formed, producing a normalized quantity M by means for dividing the difference thus formed by the sum thus formed, and means responsive to said normalized quantity M for generating delay control and reference functions for said azimuth correlator, whereby excessive azimuth bandwidth in radar echo signals is used to produce high quality spacecraft SAR images.
Claim 7
Dependent Claim 82 words
The combination of claim 5 wherein said means for generating delay control and reference functions for said azimuth correlator includes means for scaling said quantity M by a predetermined factor k, means responsive to the scaled quantity kM, a doppler frequency estimate, f, and a frequency rate, f, for generation of phase delay coefficients, means responsive to said phase delay coefficients for generation of azimuth reference coefficients, and means responsive to said phase delay coefficients for generation of range migration correction coefficients.
Claim 8
Dependent Claim 23 words
The combination of claim 5 including means connected to said correlator for registraton delay of time-multiplexed single-look image lines to produce multiple-look images.

References Cited (Backward Citations)

US4045795A Cited
US4132989A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1984-09-28 1985-03-30 1985-09-29 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1988-09-28 1989-03-30 1989-09-29 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1992-09-28 1993-03-30 1993-09-29 $7700.00 Window Closed / Lapsed

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