Two-color signature simulation using mid-infrared test source semiconductor lasers

Patent metadata

Field	Value
Publication number	US-9791558-B2
Application number	US-201514710440-A
Country	US
Kind code	B2
Filing date	May 12, 2015
Priority date	May 14, 2007
Publication date	Oct 17, 2017
Grant date	Oct 17, 2017

Abstract

In some embodiments, the present invention provides an apparatus and process that includes control electronics that generate an electronic control signal; and a plurality of optically or electrically pumped semiconductor lasers, quantum-cascade lasers, optical parametric generators, or optical parametric oscillators, operatively coupled to the control electronics, that output an optical signal having a plurality of wavelengths, each wavelength having an output intensity that each of which is varied over time to simulate a combustion signature of a weapon. In some embodiments, the optical signal includes at least two different infrared wavelengths that are varied differently with time.

First claim

What is claimed is:

1. A method comprising:
during a first time period, outputting a first laser signal having a first wavelength that has an output intensity that is varied over time to simulate a first wavelength of a combustion signature;
during the first time period, outputting a second laser signal having a second wavelength, that is different than the first wavelength, and that has an output intensity that is varied over time in a manner that is different than the intensity variation of the first wavelength, in order to simulate a second wavelength of the combustion signature, wherein the first wavelength is an infrared wavelength that is in an atmospheric-transparency window, and wherein the intensity of the second wavelength is greater than the intensity of the first wavelength for the first time period; and
generating at least one of the first laser signal and the second laser signal using an optically pumped laser.

2. The method of claim 1 , wherein the second wavelength is an infrared wavelength that is longer than the first wavelength.

3. The method of claim 1 , further comprising:
looking up an intensity value for the first laser signal for each of a plurality of successive time units in the first time period, and based on the looked-up intensity value, controlling the intensity of the first laser signal.

4. The method of claim 1 , further comprising:
varying the first laser signal intensity with a non-zero time resolution of no more than two milliseconds.

5. The method of claim 1 , further comprising:
detecting a response of a missile-warning system to the first and second laser signals; and
determining whether the response is within a specification of correct responses.

6. The method of claim 5 , wherein the detecting of the response of the missile-warning system includes detecting a countermeasure jamming signal generated by the missile-warning system in response to the first and second laser signals.

7. The method of claim 1 , wherein the first wavelength of the first laser signal is in a range of about 3.8 to 4.2 microns and the second wavelength of the second laser signal is in a range of about 4.4 to 4.8 microns.

8. The method of claim 1 , further comprising:
modulating the intensity of the first laser signal to have at least two local maximums within the first time period; and
modulating the second laser signal to have at least two local maximums within the first time period.

9. An apparatus comprising:
control electronics configured to generate a first electronic control signal and a second electronic control signal;
a first laser system operatively coupled to the control electronics, configured to output a first laser signal having a first wavelength that has an output intensity that is varied over time based on the first electronic control signal, during a first time period, to simulate a first wavelength of a combustion signature;
a second laser system operatively coupled to the control electronics, configured to output a second laser signal having a second wavelength, that is different than the first wavelength, and that has an output intensity that is varied over time based on the second electronic control signal, during the first time period, in a manner that is different than the intensity variation of the first wavelength, in order to simulate a second wavelength of the combustion signature; and
an optical element optically coupled to the first laser system and the second laser system to receive the first and second laser signal, and configured to form a far-field output beam that includes the first laser signal and the second laser signal substantially coincident with one another, wherein the first wavelength is an infrared wavelength that is in an atmospheric-transparency window, wherein the second wavelength is an infrared wavelength that is longer than the first wavelength, and wherein the intensity of the second wavelength is greater than the intensity of the first wavelength for first time period.

10. The apparatus of claim 9 , wherein at least one of the first laser signal and the second laser signal is generated by an optically pumped laser.

11. The apparatus of claim 9 , wherein at least one of the first laser signal and the second laser signal is generated by a quantum cascade laser.

12. The apparatus of claim 9 , further comprising: a look-up table operably coupled to the control electronics, wherein the look-up table is configured to provide an intensity value for the first laser signal for each of a plurality of successive time units in the first time period, wherein the intensity value is used to control the output intensity of the first laser signal.

13. The apparatus of claim 12 , wherein the first laser signal's output intensity is varied with a non-zero time resolution of no more than two milliseconds.

14. The apparatus of claim 9 , further comprising: a detector operatively coupled to the control electronics, wherein the detector is configured to detect an output response of a missile-warning system responsive to the first and second laser signals and to determine whether the output response is within a specification of correct output responses.

15. The apparatus of claim 14 , wherein the detector is configured to detect a countermeasure jamming signal generated by the missile-warning system in response to the first and second laser signals.

16. The apparatus of claim 9 , wherein the first wavelength of the first laser signal is at least 3.9 microns and no more than 4.1 microns and the second wavelength of the second laser signal is at least 4.5 microns and no more than 4.7 microns.

17. The apparatus of claim 9 , wherein the intensity of the first laser signal is modulated to have at least two local maximums within the first time period and the second laser signal is modulated to have at least two local maximums within the first time period.

18. An apparatus comprising:
means for outputting, during a first time period, a first laser signal having a first wavelength that has an output intensity that is varied over time to simulate a first wavelength of a combustion signature; and
means for outputting, during the first time period, a second laser signal having a second wavelength, that is different than the first wavelength, and that has an output intensity that is varied over time in a manner that is different than the intensity variation of the first wavelength, in order to simulate a second wavelength of the combustion signature, wherein at least one of the means for outputting the first laser signal and the means for outputting the second laser signal includes an optically pumped laser, wherein the first wavelength is an infrared wavelength that is in an atmospheric-transparency window, and wherein the intensity of the second wavelength is greater than the intensity of the first wavelength for the first time period.

19. The apparatus of claim 18 , further comprising:
means for looking up an intensity value for the first laser signal for each of a plurality of successive time units in the first time period, and means for controlling the intensity of the first laser signal based on the looked-up intensity value.

20. The apparatus of claim 18 , further comprising:
means for detecting a response of a missile-warning system to the first and second laser signals; and
means for determining whether the response is within a specification of correct responses, wherein the means for determining is operatively coupled to the means for detecting.

Assignees

• Lockheed Corp

Inventors

• Tidwell Steven C

Classifications

• F41H13/0056

  for blinding or dazzling, i.e. by overstimulating the opponent's eyes or the enemy's sensor equipment · CPC title

• F42B12/46

  for dispensing gases, vapours, powders or chemically-reactive substances (F42B12/70 takes precedence) · CPC title

• H04B10/25

  Arrangements specific to fibre transmission · CPC title

• G01S7/495 Primary

  Counter-measures or counter-counter-measures {using electronic or electro-optical means} · CPC title

• F41H11/02 Primary

  Anti-aircraft or anti-guided missile {or anti-torpedo} defence installations or systems (cartridges or missiles for producing smoke or for dispensing radar chaff or infrared material F42B5/15, F42B12/48, F42B12/70; {informative reference: details of radar or sonar systems G01S7/00; jamming or electronic countermeasures G01S7/38, G01S7/495, H04K3/00}) · CPC title