PROJECTILE TRACKING SYSTEM

• US 20090080700A1
• Filed: 06/26/2008
• Published: 03/26/2009
• Est. Priority Date: 05/25/2005
• Status: Abandoned Application

• Current Assignee: Daniel L. Lau, Michael F. Shaw
• Original Assignee: Daniel L. Lau, Michael F. Shaw
• Inventors: Shaw, Michael F., Lau, Daniel L.
• Application Number:
  US12/146,741
• Publication Number:
  US 20090080700A1
• Time in Patent Office: Days
• US Class Current: 382/103
• CPC Class Codes: F41G 3/147 based on detection of a firing weapon
• CPC Class Codes: G01S 17/66 Tracking systems using electromagnetic waves other than radio waves
• CPC Class Codes: G01S 17/86 Combinations of lidar systems with systems other than lidar, radar or sonar, e.g. with direction finders

Abstract

A system and method for determining the track of a projectile use a thermal signature of the projectile. Sequential infrared image frames are acquired from a sensor at a given position. A set of frames containing spots with characteristics consistent with a projectile in flight are identified. A possible projectile track solution for said spots is identified. A thermal signature value for each pixel of each spot of the possible solution is determined. The determined thermal signature is then compared to an actual thermal signature for a substantially similar projectile track to ascertain whether the determined thermal signature substantially matches the actual thermal signature, which indicates that the possible projectile track solution is the correct solution.

Claims

1. A method for determining the track of a projectile using a thermal signature of the projectile, said method comprising the steps of:

acquiring sequential infrared image frames from a sensor at a given position;

identifying a set of frames containing spots with characteristics consistent with a projectile in flight;

identifying at least one possible projectile track solution for said spots;

determining a projectile thermal signature value for each pixel of each spot of the possible projectile track solution;

ascertaining whether said determined projectile thermal signature substantially matches an actual projectile thermal signature for a substantially similar projectile track.

2. The method of claim 1, wherein said step of identifying a set of frames containing spots with characteristics consistent with a projectile in flight includes identifying a series of spots over several frames that:

are in a substantially straight line;

have substantially similar spacing; and

have spacing indicating a relatively fast moving object.

3. The method of claim 2, further comprising searching frames before and after said set of frames for additional spots along said substantially straight line, and including any frames containing said additional spots in said set of frames.

4. The method of claim 1, wherein said step of identifying at least one possible projectile track solution includes:

determining a centroid position of each of said spots;

determining the spacing of said spot centroid positions relative to each other; and

identifying at least one possible projectile track solution that would produce a projectile track having matching spot centroid positions.

5. The method of claim 1, wherein said step of determining a projectile thermal signature value for each pixel of each spot of the possible projectile track solution includes:

determining a measured brightness value for each pixel of each spot;

determining a background brightness value for each pixel of each spot; and

determining a projectile thermal signature value for each pixel of each spot by applying a predetermined blending function for each pixel of each spot of the possible projectile track solution to said measured brightness values and said background brightness values.

6. The method of claim 5, wherein said step of determining a background brightness value for each pixel of each spot includes averaging the brightness values of the pixels that correspond to the pixels of each spot in the set of frames that do not contain the respective spots.

7. The method of claim 5, wherein said predetermined blending function is a second-order Taylor Series expansion of the measured brightness value into intensity of the infrared radiation attributable to the projectile and the intensity of the infrared radiation attributable to the background.

8. A system for determining the track of a projectile using a thermal signature of the projectile, said system comprising:

an infrared sensor for acquiring sequential infrared image frames;

a database component relating projectile thermal signature values for each pixel of each spot for projectile tracks detectable by said infrared sensor; and

a processing component, operatively connected to said database component and said infrared sensor, for;

identifying a set of frames containing spots with characteristics consistent with a projectile in flight;

identifying at least one possible projectile track solution for said spots;

determining a projectile thermal signature value for each pixel of each spot of the possible projectile track solution; and

ascertaining whether said determined projectile thermal signature substantially matches an actual projectile thermal signature from said database component for a substantially similar projectile track.

9. The system of claim 8, wherein said processing component comprises a projectile detection element and a track determination element, said projectile detection element for identifying said set of frames containing spots with characteristics consistent with a projectile in flight, and said track determination element for:

identifying at least one possible projectile track solution for said spots;

determining a projectile thermal signature value for each pixel of each spot of the possible projectile track solution; and

ascertaining whether said determined projectile thermal signature substantially matches an actual projectile thermal signature from said database component for a substantially similar projectile track.

10. The system of claim 8, wherein said processing component is further for identifying a series of spots over several frames that:

are in a substantially straight line;

have substantially similar spacing; and

have spacing indicating a relatively fast moving object.

11. The system of claim 10, wherein said processing component is further for searching frames before and after said set of frames for additional spots along said substantially straight line, and including any frames containing said additional spots in said set of frames.

12. The system of claim 8, wherein said processing component is further for:

determining a centroid position of each of said spots;

determining the spacing of said spot centroid positions relative to each other;

identifying at least one possible projectile track solution that would produce a projectile track having matching spot centroid positions.

13. The system of claim 8, wherein said processing component is further for:

determining a measured brightness value for each pixel of each spot;

determining a background brightness value for each pixel of each spot; and

determining a projectile thermal signature value for each pixel of each spot by applying a predetermined blending function for each pixel of each spot of the possible projectile track solution to said measured brightness values and said background brightness values.

14. The system of claim 13, wherein said predetermined blending function is a second-order Taylor Series expansion of the measured brightness value into intensity of the infrared radiation attributable to the projectile and the intensity of the infrared radiation attributable to the background.

15. The system of claim 8, further comprising a graphical user interface component operatively connected to said processing component for presenting a final projectile track solution to a user.

16. The system of claim 15, further comprising a visible light sensor positioned so as to have a field of view that overlaps a field of view of said infrared sensor, said visible light sensor operatively connected to said graphical user interface component, said graphical user interface component further for overlaying an infrared image from said infrared sensor with a visible image from said visible light sensor for providing said user with a visible light context for said infrared image.

17. The system of claim 8, further comprising a position/direction component proximate said infrared sensor, said position/direction component operatively connected to said processing component for providing an actual global position and direction of said infrared sensor to said processing component, said processing component further for providing an actual global projectile track solution, including the actual global location from which the projectile was fired.

18. The system of claim 8, further comprising an active target designator unit operatively connected to said processing component for designating and tracking the projectile using a final projectile track solution.

19. A computer readable medium having computer executable instructions for performing a method for determining the track of a projectile using a thermal signature of the projectile, said method comprising the steps of:

acquiring sequential infrared image frames from a sensor at a given position;

identifying a set of frames containing spots with characteristics consistent with a projectile in flight;

identifying at least one possible projectile track solution for said spots;

determining a projectile thermal signature value for each pixel of each spot of the possible projectile track solution;

ascertaining whether said determined projectile thermal signature substantially matches an actual projectile thermal signature for a substantially similar projectile track.

20. The computer readable medium of claim 19, wherein said computer executable instructions for performing said step of identifying a set of frames containing spots with characteristics consistent with a projectile in flight includes computer executable instructions for identifying a series of spots over several frames that:

are in a substantially straight line;

have substantially similar spacing; and

have spacing indicating a relatively fast moving object.

21. The computer readable medium of claim 20, further having computer executable instructions for searching frames before and after said set of frames for additional spots along said substantially straight line, and including any frames containing said additional spots in said set of frames.

22. The computer readable medium of claim 19, wherein said computer executable instructions for performing said step of identifying at least one possible projectile track solution include computer executable instructions for:

determining a centroid position of each of said spots;

determining the spacing of said spot centroid positions relative to each other; and

identifying at least one possible projectile track solution that would produce a projectile track having matching spot centroid positions.

23. The computer readable medium of claim 19, wherein said computer executable instructions for performing said step of determining a projectile thermal signature value for each pixel of each spot of the possible projectile track solution include computer executable instructions for:

determining a measured brightness value for each pixel of each spot;

determining a background brightness value for each pixel of each spot; and

determining a projectile thermal signature value for each pixel of each spot by applying a predetermined blending function for each pixel of each spot of the possible projectile track solution to said measured brightness values and said background brightness values.

24. The computer readable medium of claim 23, wherein said computer executable instructions for applying a blending function include computer executable instructions for applying a second-order Taylor Series expansion of the measured brightness value into intensity of the infrared radiation attributable to the projectile and the intensity of the infrared radiation attributable to the background.

25. A method of building a projectile thermal signature record comprising the steps of:

(a) selecting an initial projectile track;

(b) aiming the field of view of an infrared sensor at a portion of a path of travel of said projectile track;

(c) repeatedly shooting projectiles in said projectile track in a first environmental condition;

(d) recording infrared images of said projectiles of step (c);

(e) repeatedly shooting projectiles in said projectile track in a second environmental condition that has a substantially different ambient temperature from said first environmental condition;

(f) recording infrared images of said projectiles of step (e);

(g) determining a projectile thermal signature value for each pixel corresponding to a position along said projectile track by;

using a blending function to characterize the measured brightness value of each pixel as a blend of the infrared radiation attributable to the projectile and the infrared radiation attributable to the background;

setting the average values of the radiation attributable to the projectile for each pixel of each set of images equal to one other;

solving for the unknown values of the blending function for each pixel corresponding to a position along said projectile track; and

solving for the projectile thermal signature value for each pixel corresponding to a position along said projectile track;

(h) moving said infrared sensor to another portion of said path of travel of said projectile track and repeating steps (c) through (h) until the full path of travel of said projectile track is documented; and

(i) selecting another projectile track and repeating steps (b) through (i) until blended function values and projectile thermal signature values are determined for observable solution tracks.

26. The method of claim 25, wherein said blending function is a second-order Taylor Series expansion of the measured brightness value into intensity of the infrared radiation attributable to the projectile and the intensity of the infrared radiation attributable to the background