High-resolution imaging and target designation through clouds or smoke

• US 6,515,737 B2
• Filed: 01/03/2001
• Issued: 02/04/2003
• Est. Priority Date: 01/04/2000
• Status: Expired due to Fees

• Current Assignee: Lawrence Livermore National Security LLC (Government of the United States of America)
• Original Assignee: Regents of the University of California (University of California)
• Inventors: Perry, Michael D.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): ANDREA, BRIAN K
• Application Number:
  US09/754,884
• Publication Number:
  US 20020005942A1
• Time in Patent Office: 762 Days
• Field of Search: 356/3-1-, 356/5.03, 356/5.04, 348/144-147, 348/31
• US Class Current: 356/5.04
• CPC Class Codes: F41G 7/263 Means for producing guidance beams
• CPC Class Codes: G01S 17/66 Tracking systems using electromagnetic waves other than radio waves
• CPC Class Codes: G01S 7/481 Constructional features, e.g. arrangements of optical elements

Abstract

A method and system of combining gated intensifiers and advances in solid-state, short-pulse laser technology, compact systems capable of producing high resolution (i.e., approximately less than 20 centimeters) optical images through a scattering medium such as dense clouds, fog, smoke, etc. may be achieved from air or ground based platforms. Laser target designation through a scattering medium is also enabled by utilizing a short pulse illumination laser and a relatively minor change to the detectors on laser guided munitions.

Claims

1. A method comprising:

generating pulsed electromagnetic radiation having a predetermined wavelength selected from the ranges consisting of from about 350 to 380 nm and from about 850 to about 1100 nm through a scattering medium toward a target;

receiving reflections of said pulsed electromagnetic radiation through said scattering medium from said target; and

forming a temporally gated image of the target consisting essentially of a ballistic component of the reflected pulsed electromagnetic radiation.

2. A method comprising:

generating pulsed electromagnetic radiation from an aircraft having a predetermined wavelength selected from the ranges consisting of from about 350 to about 380 nm and from about 850 to about 1100 nm through a scattering medium towards a ground-based target;

receiving reflections of said pulsed electromagnetic radiation at said aircraft through said scattering medium from said ground-based target; and

forming a temporally gated image of the target consisting essentially of a ballistic component of the reflected pulsed electromagnetic Radiation.

3. A method comprising:

generating pulsed electromagnetic radiation from an aircraft having a predetermined wavelength selected from the ranges consisting of from about 350 to about 380 nm and from about 850 to about 1100 nm through a scattering medium towards a ground-based target;

receiving reflections of said pulsed electromagnetic radiation at said aircraft through said scattering medium from said ground-based target; and

collecting the reflected pulsed electromagnetic radiation consisting essentially of a ballistic component on the aircraft.

4. A method comprising:

generating an illuminator pulse of electromagnetic through a scattering medium towards a target located at a distance greater than approximately 1000 feet;

receiving a reflection of said illuminator pulse through said scattering medium from said ground-based target; and

collecting the reflected illuminator pulse consisting essentially of a ballistic component at a gated temporal sensor.

5. An apparatus comprising:

a means for generating pulsed electromagnetic radiation having a predetermined wavelength selected from the ranges consisting of from about 350 to about 380 nm and from about 850 to about 1100 nm through a scattering medium towards a target;

a means for receiving reflections of said pulsed electromagnetic radiation through said scattering medium from said target; and

a means for forming a temporally gated image of the target consisting essentially of a ballistic component of the reflected pulsed electromagnetic radiation.

6. An apparatus comprising:

a means for generating pulsed electromagnetic radiation from an aircraft having a predetermined wavelength selected from the ranges consisting of from about 350 to about 380 nm and from about 850 to about 1100 nm through a scattering medium towards a ground-based target;

a means for receiving reflections of said pulsed electromagnetic radiation at said aircraft through said scattering medium from said ground-based target; and

a means for forming a temporally gated image of the target on the aircraft consisting essentially of a ballistic component of the reflected pulsed electromagnetic Radiation.

7. An apparatus comprising:

a means for generating pulsed electromagnetic radiation from an aircraft having a predetermined wavelength selected from the ranges consisting of from about 350 to about 380 nm and from about 850 to about 1100 nm through a scattering medium towards a ground-based target;

a means for receiving reflections of said pulsed electromagnetic radiation at said aircraft through said scattering medium from said ground-based target; and

a means for collecting the reflected pulsed electromagnetic radiation consisting essentially of a ballistic component on the aircraft.

8. A method comprising:

generating a trigger pulse and an illuminator pulse of electromagnetic radiation from an aircraft through a scattering medium towards a ground-based target;

receiving a reflection of the trigger pulse from said scattering medium at said aircraft to determine the distance from the aircraft to the scattering medium;

receiving a reflection of the trigger pulse from said ground based-target at said aircraft to determine the distance from the aircraft to the ground-based target and to turn on a sensor on said aircraft;

receiving a reflection of said illuminator pulse at said aircraft through said scattering medium from said ground-based target; and

collecting the ballistic component of the reflected illuminator pulse at said sensor.

9. The method of claim 8, wherein said sensor is turned on by said trigger pulse for approximately 4 to 10 nsec.

10. The method of claim 8, wherein said sensor is turned on by said trigger pulse for less than approximately 6 nsec.

11. The method of claim 8, wherein said illuminator pulse is generated with a predetermined wavelength between approximately 350 to 380 nm.

12. The method of claim 8, wherein said illuminator pulse is generated with a predetermined wavelength between approximately 850 to 1100 nm.

13. The method of claim 8, further comprising:

creating a delay between the trigger pulse and the illuminator pulse.

14. The method according to claim 13, wherein said delay is less than 6 nsec.

15. A method comprising:

generating a trigger pulse and an illuminator pulse of electromagnetic radiation from an aircraft through a scattering medium towards a target located at a distance greater than approximately 1000 feet;

receiving a reflection of the trigger pulse from said target to turn on a sensor;

receiving a reflection of said illuminator pulse through said scattering medium from said target; and

collecting the ballistic component of the reflected illuminator pulse at said sensor.

16. An apparatus comprising:

a laser capable of producing a pulse;

a beam splitter coupled to said laser to divide the pulse into a trigger pulse and an illuminator pulse;

a delay section capable of creating a delay between the trigger pulse and the illuminator pulse;

a variable telescope coupled to said delay section and capable of controlling the divergence of the illuminator pulse;

a photodiode capable of receiving a reflection of said trigger pulse from a target;

an acquisition mirror capable of receiving a reflection of said illumination pulse from said target; and

a gated intensifier which is turned on by said reflection of said trigger pulse and which collects image information on the target from said reflection of said illumination pulse from said target.

17. The apparatus of claim 16, wherein said gated intensifier includes at least one from the group consisting of a photocathode, a microchannel plate, a phosphor screen, a fiber optic taper and a charge-coupled device (CCD).

18. The apparatus of claim 16, further comprising:

a primary mirror optically coupled to said acquistion mirror and said gated intensifier.

19. The apparatus of claim 16, wherein said delay is less than 6 nsec.

20. An aircraft mounted apparatus comprising:

a laser capable of producing a pulse;

a beam splitter coupled to said laser to divide the pulse into a trigger pulse and an illuminator pulse;

a delay section capable of creating a delay between the trigger pulse and the illuminator pulse;

a variable telescope coupled to said delay section and capable of controlling the divergence of the illuminator pulse;

a photodiode capable of receiving a reflection of said trigger pulse from a ground-based target;

an acquisition mirror capable of receiving a reflection of said illumination pulse from said target; and

a gated intensifier which is turned on by said reflection of said trigger pulse and which collects image information on the target from said reflection of said illumination pulse from said target.

21. The aircraft mounted apparatus of claim 20, wherein said gated intensifier is capable of producing optical images having a resolution of less than approximately 20 centimeters.