Hyperspectral infrared sounders deployable as a constellation for low orbit MWIR atmospheric measurements

• US 10,444,145 B2
• Filed: 05/03/2016
• Issued: 10/15/2019
• Est. Priority Date: 05/04/2015
• Status: Active Grant

• Current Assignee: BAE Systems Information and Electronic Systems Integration Incorporated (BAE Systems Plc)
• Original Assignee: BAE Systems Information and Electronic Systems Integration Incorporated (BAE Systems Plc)
• Inventors: Maschhoff, Kevin R., Perron, Gerard M., Polizotti, John J.
• Primary Examiner(s): Taningco, Marcus H
• Application Number:
  US15/571,197
• Publication Number:
  US 20190154576A1
• Time in Patent Office: 1,260 Days
• CPC Class Codes: G01J 2005/202 Arrays
• CPC Class Codes: G01J 3/18 using diffraction elements, e.g. grating gratings per se G02B
• CPC Class Codes: G01J 3/2823 Imaging spectrometer
• CPC Class Codes: G01J 5/007 for earth observation
• CPC Class Codes: G01J 5/0205 Mechanical elements; Supports for optical elements
• CPC Class Codes: G01J 5/041 Mountings in enclosures or in a particular environment
• CPC Class Codes: G01J 5/061 by controlling the temperature of the apparatus or parts thereof, e.g. using cooling means or thermostats
• CPC Class Codes: G01J 5/20 using resistors, thermistors or semiconductors sensitive to radiation, e.g. photoconductive devices
• CPC Class Codes: G01N 2021/1793 Remote sensing
• CPC Class Codes: G01N 2021/3531 without instrumental source, i.e. radiometric
• CPC Class Codes: G01N 21/3518 Devices using gas filter correlation techniques; Devices using gas pressure modulation techniques
• CPC Class Codes: G01N 21/3554 for determining moisture content
• CPC Class Codes: G01N 21/41 Refractivity; Phase-affecting properties, e.g. optical path length G01N21/21 takes precedence
• CPC Class Codes: G01W 1/04 giving only separate indications of the variables measured
• CPC Class Codes: H01L 31/107 the potential barrier working in avalanche mode, e.g. avalanche photodiodes

Abstract

A mid-wave infrared system provides high spatial and temporal resolution measurements of atmospheric temperatures and moisture fields using a constellation of low earth orbit satellites. The disclosed system is smaller, lighter, less complex, and requires less energy than existing systems, due to implementation of an infrared avalanche photodiode array detector that provides enhanced sensitivity with reduced cooling requirements, and an Offner spectrometer having a novel a refractive element inserted near the grating that reduces the size and power requirements of the spectrometer. Embodiments of the disclosed method include deploying a constellation of devices for cooperative infrared sensing of atmospheric phenomena at similar rates, lower cost, and much higher resolution compared to geosynchronous approaches. Some embodiments further include combined analysis of measurements obtained by the disclosed devices with complementary measurements made by other low-earth and high-earth orbital and/or ground-based devices.

Claims

1. A device suitable for making infrared atmospheric measurements, the device comprising:

an avalanche infrared photodiode array;

a cryo-cooler configured to cool the photodiode array;

a spectrometer having an Offner architecture, said spectrometer including a grating and a refractive element proximal to the grating;

an optical and self-emission baffle; and

a two-zone passive thermal radiator having a first zone configured to cool the baffle while in orbit and a second zone configured to cool the spectrometer while in orbit.

2. The device of claim 1, wherein the cryo-cooler is configured to cool the photodiode array to a temperature that is between 75K and 100K.

3. The device of claim 2, wherein the cryo-cooler is able to cool the photodiode to a temperature below 100K while consuming less than 15 W of power.

4. The device of claim 1, wherein the cryo-cooler is an NGST miniature pulse-tube cooler that has a specific cooling power of at least 20 W/W at 100K.

5. The device of claim 1, wherein the first zone of the two-zone radiator is able to cool the baffle to a temperature that is between 175K and 195K.

6. The device of claim 1, wherein the spectrometer is limited to detecting infrared radiation in the range of 1950 cm⁻

1 to 2450 cm<sup>−

1</sup>.

7. The device of claim 1, wherein the spectrometer is configured to detect water vapor absorption lines in the range of 1950-2325 cm⁻

1.

8. The device of claim 1, wherein the spectrometer has a minimum resolution of less than 2.3 cm⁻

1.

9. The device of claim 1, wherein the spectrometer has a radiometric sensitivity threshold of less than 200 mK.

10. The device of claim 1, wherein the device has a total weight of less than 12 kg.

11. The device of claim 1, wherein the device has a total power consumption requirement of less than 40 W.

12. The device of claim 1, further comprising an on-board spectral data handling system that employs an FPGA-based processing chain.

13. A method of making hyperspectral soundings of the earth'"'"'s atmosphere from a constellation of earth satellites, the method comprising:

deploying a plurality of satellites in a constellation of orbits surrounding the earth, wherein a device as described in claim 1 is included with each of the satellites; and

obtaining from the devices cooperative distributed infrared sensing measurements of atmospheric phenomena.

14. The method of claim 13, wherein the satellites are deployed in low earth orbit at an altitude of approximately 705 km above the earth'"'"'s surface.

15. The method of claim 13, wherein the constellation is able to make observations of a region that are repeated every 90 minutes.

16. The method of claim 13, wherein the constellation is able to make repeated observations of a region with a repetition interval of less than fifteen minutes.

17. The method of claim 13, wherein observations obtained from the constellation are provided together with observations obtained from other devices as input for at least one of atmospheric modeling and weather forecasting.