IP Library Granted Patent US 9,212,968
Granted Patent B1
US 9,212,968 · App. 14/012,202 · Granted Dec 15, 2015

Onboard calibration source for spectral calibraton of a radiometer

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Quick Facts
Patent No.
US 9,212,968
App. No.
14/012,202
Granted
Dec 15, 2015
Kind
B1
Abstract

A calibration device for a radiometer includes an integrating cavity and a honeycomb blackbody mounted to the integrating cavity. A plurality of emitters are mounted to the exterior rim of the integrating cavity for transmitting narrow band wavelengths of light into and out of the integrating cavity. A controller, selectively, activates one or more emitters to radiate a single narrow band wavelength of light during an ON period and turn OFF during another period. A plurality of reference detectors are also mounted to the exterior rim of the integrating cavity for measuring the intensity of each narrow band radiation outputted from the integrating cavity. The reference detectors are effective in determining changes in intensity output by each of the narrow band emitters from the integrating cavity. The measured changes in intensity outputted by the emitters are used to calibrate the radiometer with the changes traced back to a NIST standard.

Claims (64)

1. A calibration device for a radiometer comprising:

a housing disposed in an orbiting satellite for passing light to an imaging device,

a plurality of emitters disposed in the housing for transmitting light toward the imaging device, and

a plurality of detectors disposed in the housing for receiving a portion of the light transmitted toward the imaging device,

wherein the emitters are configured to transmit narrow band wavelengths of light in the visible spectral region, and

the detectors are configured to measure a change in radiance of the light transmitted toward the imaging device.

2. The calibration device of claim 1 wherein

the imaging device includes an Earth observation instrument including a telescope.

3. The calibration device of claim 1 wherein

the emitters include at least one of a blue emitting diode, a green emitting diode and a red emitting diode.

4. The calibration device of claim 1 wherein

the emitters include at least one of a 445 nanometer light emitting diode (LED), a 665 nanometer LED, and a 980 nanometer LED.

5. The calibration device of claim 1 wherein

the emitters include at least one of a 1.0 micron LED and a 1.5 micron LED.

6. The calibration device of claim 1 wherein

the detectors include at least one of a silicon PIN diode and an InGaAs photo-diode.

7. The calibration device of claim 1 wherein

the detectors are configured to be calibrated by a standard in a ground laboratory, and

the emitters are configured to monitor changes in the detectors when disposed in the orbiting satellite.

8. The calibration device of claim 7 wherein

the emitters include an LED transmitting light in the visible spectrum having a wavelength below 800 nanometers, and

the detectors include a silicon PIN diode.

9. The calibration device of claim 1 further comprising:

a honeycomb blackbody and an integrating cavity,

wherein the emitters are configured to radiate light into the integrating cavity,

the integrating cavity is configured to reflect received light toward the honeycomb blackbody, and

the honeycomb blackbody is configured to pass the reflected light toward the imaging device.

10. The calibration device of claim 9 further comprising:

a controller for pulsing each of the emitters ON/OFF,

wherein a respective emitter is configured to radiate a respective narrowband wavelength of visible light and thermal radiation during the respective emitter's ON time, and

configured to radiate thermal radiation during the respective emitter's OFF time.

11. The calibration device of claim 9 wherein

the honeycomb blackbody is configured to radiate infrared light toward the imaging device.

12. The calibration device of claim 1 wherein

the imaging device is configured to view the Earth, and

the imaging device is configured to view the housing including the light transmitted from each of the emitters.

13. A calibration device for a radiometer comprising:

an integrating cavity for outputting received light, the integrating cavity including a semi-spherical surface terminating in a flat surface,

a honeycomb blackbody mounted to the flat surface for radiating infrared light, and

a plurality of emitters mounted to the semi-spherical surface for transmitting visible light into the integrating cavity,

wherein the radiometer is configured to selectively view the infrared light and the visible light during calibration of the radiometer.

14. The calibration device of claim 13 further comprising:

a plurality of detectors mounted to the semi-spherical surface for detecting light outputted from the integrating cavity,

wherein the detectors measure a change in intensity of the light outputted from the integrating cavity.

15. The calibration device of claim 14 wherein

the emitters include at least one of a blue wavelength LED, a green wavelength LED, a red wavelength LED, a 1.0 micron wavelength LED and a 1.5 micron laser diode, and

the detectors include at least one of a silicon PIN diode and an InGaAs detector.

16. The calibration device of claim 14 wherein

the radiometer includes an Earth viewing instrument, and

the instrument is positioned to view the visible and infrared light during calibration.

17. The calibration device of claim 14 further comprising:

a controller for pulsing each of the emitters ON/OFF,

wherein during an ON time of a respective emitter, the radiometer views visible and infrared light, and

during an OFF time of the respective emitter, the radiometer views infrared light.

18. The calibration device of claim 13 wherein

the radiometer is an Earth viewing instrument, and

the emitters are disposed in an Earth orbiting satellite.

19. A method of calibrating a telescope comprising the steps of:

transmitting narrowband wavelengths of visible light from an integrating cavity, wherein the transmitted visible light is radiated from a respective diode and passed through a honeycomb blackbody;

selectively configuring the telescope to view the transmitted visible light; and

monitoring the transmitted visible light from the integrating cavity using at least one reference detector, wherein the detector is configured to measure intensity change in a respective narrowband wavelength of light transmitted from the respective diode.

20. The method of claim 19 including the steps of:

pulsing the transmitted visible light ON/OFF, wherein each transmitted visible light is individually pulsed ON/OFF; and

monitoring each respective narrowband wavelength of light transmitted during an ON time and subtracting thermal radiation transmitted from the respective diode during an OFF time.

Assignments (2)
MERGER Recorded Jul 1, 2016
From: EXELIS INC.
To: HARRIS CORPORATION
Reel/Frame 039362/0534 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 28, 2013
From: WICKHOLM, DAVID R.; SMITH, DAVID S.; GLUMB, RONALD JOSEPH; STOKES, SHELDON; WHITE, GLEN DANIEL
To: EXELIS, INC.
Reel/Frame 031101/0269 →