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US5103484A Expired / Lapsed US ⏱️ 0.0 years remaining

Target aimpoint location

Assignee: Matra Bae Dynamics UK Ltd
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Filing: 1991-05-08
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Granted: 1992-04-07
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Expires: 2011-05-08
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Abstract

Abstract This invention relates to a method for analyzing a viewed scene containing a target. The scene is digitized forming a binary image in which the target is distinguished from the background. The image is then processed to form a contoured representation of the target, and a target skeleton. Finally a contoured skeleton is produced and the target aimpoint is determined.

Inventors

  • 👤 Raymond J. P. Stafford
  • 👤 Enoch James

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 12:51
CPC Classifications
F; F41; F41G; F41G7/00; F41G7/20; F41G7/22; F41G7/2226; F41G7/2253; F41G7/2273; F41G7/2293; G; G01; G01S; G01S3/00; G01S3/78; G01S3/782; G01S3/785; G01S3/786; G01S3/7864

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 173 words
A method of determining a target aimpoint in a missile guidance tracking system, the method comprising the steps of: (a) forming an image of a viewed scene; (b) determining the presence of a target in the image; (c) digitizing said image to form a binary image; said binary image comprising a two-dimensional array of pixels distinguishing a target image from other elements of the image; (d) forming a contoured image of the target image from said binary image by assigning weights to said pixels based on a location of a pixel relative to edges of the target image; (e) forming a skeleton image of the target image from said binary image by selecting pixels based on a location of a pixel relative to said edges of the target image; (f) forming a contoured skeleton image by assigning the assigned weights of pixels in said contoured image to the corresponding pixels in said skeleton image; and (g) processing the assigned weights of the pixels in said contoured skeleton image to determine the target aimpoint.
Claim 2
Independent Claim 173 words
A method of determining a target aimpoint in a missile guidance tracking system, the method comprising the steps of: (a) forming an image of a viewed scene; (b) determining the presence of a target in the image; (c) digitizing said image to form a binary image; said binary image comprising a two-dimensional array of pixels distinguishing a target image from other elements of the image; (d) forming a contoured image of the target image from said binary image by assigning weights to said pixels based on a location of a pixel relative to edges of the target image; (e) forming a skeleton image of the target image from said binary image by selecting pixels based on a location of a pixel relative to said edges of the target image; (f) forming a contoured skeleton image by assigning the assigned weights of pixels in said contoured image to the corresponding pixels in said skeleton image; and (g) processing the assigned weights of the pixels in said contoured skeleton image to determine the target aimpoint.
Claim 3
Dependent Claim 20 words
The method of claim 1, wherein in said target aimpoint is determined as the centroid of said contoured skeleton image.
Claim 4
Dependent Claim 47 words
A method according to claim 2, wherein the centroid is determined based on a chosen pixel of said contoured skeleton image, the weights of the respective pixels of said contoured skeleton image, and a distance of each pixel in said contoured skeleton image from said chosen pixel.
Claim 5
Dependent Claim 22 words
The method of claim 3, wherein said chosen pixel is the pixel in said contoured skeleton image with the highest pixel weight.
Claim 6
Dependent Claim 36 words
A method according to claim 1, wherein said contoured image is formed by assigning each pixel in the target image a value according to the distance of a pixel from said edges of the target image.
Claim 7
Dependent Claim 24 words
A method according to claim 1, wherein said skeleton image is formed by applying a set of predetermined test conditions to said binary image.

References Cited (Backward Citations)

US3339179A Cited
US4405940A Cited
US4409661A Cited
US4739401A Cited
US4796187A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1995-04-07 1995-10-07 1996-04-07 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1999-04-07 1999-10-07 2000-04-07 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2003-04-07 2003-10-07 2004-04-07 $7700.00 Window Closed / Lapsed

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