Light emitting diodes for simulation of missile signatures

Patent metadata

Field	Value
Publication number	US-9267770-B2
Application number	US-201213625363-A
Country	US
Kind code	B2
Filing date	Sep 24, 2012
Priority date	Sep 22, 2011
Publication date	Feb 23, 2016
Grant date	Feb 23, 2016

Abstract

An emitting structure for simulating an irradiance signature of a missile is provided. The emitting structure includes one or more radiation sources, each of which includes at least one ultraviolet radiation source and at least one infrared radiation source. The emitting structure also includes a spherical shell and a mechanism for positioning the radiation source(s) along a three dimensional boundary of the spherical shell. The emitting structure can locate and operate one of the radiation sources to simulate the irradiance signature of the missile.

First claim

What is claimed is:

1. A system comprising:
an emitting structure including:
a first radiation source including at least one ultraviolet radiation source and at least one infrared radiation source, wherein the first radiation source further includes: a reflective enclosure surrounding the at least one ultraviolet radiation source and the at least one infrared radiation source; and means for moving the at least one ultraviolet radiation source and the at least one infrared radiation source with respect to the reflective enclosure;
a spherical shell; and
means for positioning the first radiation source along a three dimensional boundary of the spherical shell; and

a computer system for simulating an irradiance signature of a missile using the first radiation source and the means for positioning, wherein the simulating includes, for each of a plurality of simulation times:
determining a relative location of the simulated missile with respect to a target location;
determining a plume irradiance appearance at the target location based on the relative location, a missile type for the missile, and a set of missile operating conditions for the missile;
locating the first radiation source to a location on the spherical shell corresponding to the relative location; and
generating a radiation pattern simulating the plume irradiance appearance using the first radiation source.

2. The system of claim 1 , wherein the first radiation source further includes a visible radiation source.

3. The system of claim 1 , wherein the emitting structure further includes:
a second radiation source including at least one ultraviolet radiation source and at least one infrared radiation source, wherein the first radiation source generates radiation using a first pattern and the second radiation source generates radiation using a second pattern distinct from the first pattern; and
a second means for positioning the second radiation source along the three dimensional boundary of the spherical shell, wherein the simulating further includes selecting the first radiation source based on the first pattern matching the plume irradiance appearance better than the second pattern.

4. The system of claim 1 , wherein the at least one ultraviolet radiation source includes:
a first ultraviolet light emitting diode configured to emit ultraviolet radiation having a peak wavelength centered around approximately 0.27 microns;
a second ultraviolet light emitting diode configured to emit ultraviolet radiation having a peak wavelength centered around approximately 0.28 microns; and
a third ultraviolet light emitting diode configured to emit ultraviolet radiation having a peak wavelength centered around approximately 0.29 microns.

5. The system of claim 1 , wherein the at least one infrared radiation source includes a first infrared light emitting diode configured to emit infrared radiation having a peak wavelength centered around approximately 4.5 microns.

6. The system of claim 5 , wherein the at least one infrared radiation source further includes:
a second infrared light emitting diode configured to emit infrared radiation having a peak wavelength centered around approximately 2.45 microns;
a third infrared light emitting diode configured to emit infrared radiation having a peak wavelength centered around approximately 3.0 microns; and
a fourth infrared light emitting diode configured to emit infrared radiation having a peak wavelength centered around approximately 4.2 microns.

7. The system of claim 1 , further comprising a detector located at a center of the spherical shell, wherein the target location corresponds to a simulated location of the detector.

8. The system of claim 7 , wherein the system includes a plurality of emitting structures, each with a corresponding detector, and wherein the simulating evaluates an ability of the detectors to track the missile.

9. A system comprising:
a plurality of emitting structures, each emitting structure including:
a first radiation source including at least one ultraviolet radiation source and at least one infrared radiation source;
a spherical shell; and
means for positioning the first radiation source along a three dimensional boundary of the spherical shell;

a plurality of detectors, each detector located at a center of the spherical shell of one of the plurality of emitting structures; and
a computer system for simulating, for each of the plurality of detectors, an irradiance signature of a missile at the detector using the first radiation source and the means for positioning of the corresponding emitting structure, wherein the simulating includes, for each of the plurality of detectors and a plurality of simulation times:
determining a relative location of the simulated missile with respect to a simulated position of the detector;
determining a plume irradiance appearance at the detector based on the relative location, a missile type for the missile, and a set of missile operating conditions for the missile;
locating the first radiation source to a location on the spherical shell corresponding to the relative location; and
generating a radiation pattern simulating the plume irradiance appearance using the first radiation source.

10. The system of claim 9 , wherein each of the plurality of emitting structures further includes:
a second radiation source including at least one ultraviolet radiation source and at least one infrared radiation source, wherein the first radiation source generates radiation using a first pattern and the second radiation source generates radiation using a second pattern distinct from the first pattern; and
a second means for positioning the second radiation source along the three dimensional boundary of the spherical shell, wherein the simulating further includes, for each of the plurality of emitting structures, selecting the first radiation source based on the first pattern matching the plume irradiance appearance better than the second pattern.

11. The system of claim 9 , wherein the simulating evaluates an ability of the detectors to track the missile using triangulation.

12. The system of claim 9 , wherein the simulating evaluates an ability of one of the plurality of detectors to handoff tracking the missile to another one of the plurality of detectors.

13. The system of claim 9 , wherein each of the plurality of emitting structures further includes means for optically communicating with at least one other emitting structure during the simulating.

14. A system comprising:
an emitting structure including:
a plurality of radiation sources, each radiation source including at least one ultraviolet radiation source and at least one infrared radiation source having a unique pattern;
a spherical shell; and
means for positioning the plurality of radiation sources along a three dimensional boundary of the spherical shell; and

a computer system for simulating an irradiance signature of a missile using one of the plurality of radiation sources and the means for positioning, wherein the simulating includes:
selecting one of the plurality of radiation sources based on the irradiance signature and the unique pattern for each of the plurality of radiation sources; and

for each of a plurality of simulation times:
determining a relative location of the simulated missile with respect to a target location;
determining a plume irradiance appearance at the target location based on the relative location, a missile type for the missile, and a set of missile operating conditions for the missile;
locating the selected radiation source to a location on the spherical shell cor

Assignees

• Sensor Electronic Tech Inc

Inventors

• Gaska Remigijus
• Dobrinsky Alexander
• Shatalov Maxim
• Shur Michael

Classifications

• F41H11/02

  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

• F41J9/08

  Airborne targets, e.g. drones, kites, balloons {(aircraft for towing targets B64D3/02)} · CPC title

• F41J2/00 Primary

  Reflecting targets, e.g. radar-reflector targets; Active targets transmitting electromagnetic {or acoustic} waves · CPC title

• F41J9/00

  Moving targets, i.e. moving when fired at (F41J2/00 takes precedence) · CPC title

• F41G7/002

  target simulators · CPC title