Spectral drift and correction technique for hyperspectral imaging systems

• US 20020015151A1
• Filed: 07/26/2001
• Published: 02/07/2002
• Est. Priority Date: 07/27/2000
• 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: Gorin, Brian A.
• Granted Patent: US 6,819,798 B2
• Time in Patent Office: Days
• US Class Current: 356/303
• CPC Class Codes: G01J 2003/2826 Multispectral imaging, e.g. filter imaging
• CPC Class Codes: G01J 2003/2866 Markers; Calibrating of scan
• CPC Class Codes: G01J 3/2823 Imaging spectrometer

Abstract

A method for determining magnitude and direction of spectral channel drift for several consecutive spectral regions over a wide spectral range. According to the method of the present invention, in-field testing of a spectral filter sequentially irradiated by two blackbody sources is performed to generate a response function of the spectral filter. The response function is ensemble averaged to reduce any noise. Background radiance is then removed to produce a smoothed spectral transmittance function of the spectral filter. The first derivative function of the smoothed spectral transmittance function is determined. The first derivative function is separated into spectral band regions having +/− N pixels on either side of the function minima. The value of N is selected to optimize the detection algorithm sensitivity to change while extending the limit of spectral shift magnitude. The sum of the differences between the first derivative function and a reference spectral derivative function is determined. The difference result is applied to a look-up table to determine magnitude and direction of spectral drift for each of the separated spectral band regions. Use of the present invention can provide information on spectral distortion or spectral smile for 2-D focal plane arrays used for hyperspectral imaging.

Claims

1. A method for detecting spectral drift in a hyperspectral imaging system, comprising the steps of:

(a) obtaining in-field measurements of a response function for a calibration filter;

(b) obtaining in-field measurements of a response function for an onboard blackbody;

(c) determining a spectral transmittance function using said response functions from steps (a) and (b) for said calibration filter and said onboard blackbody;

(d) determining a first derivative function of said spectral transmittance function;

(e) separating said first derivative function into a plurality of spectral band regions, each of said spectral band regions having +/−

N pixels on either side of a localized minima;

(f) determining a pixel shift magnitude value for one of said plurality of spectral band regions; and

(g) applying said pixel shift magnitude value to a look-up table to determine a magnitude and direction of said spectral drift for one of said plurality of spectral band regions.

2. The method of claim 1, wherein step (a) comprises the step of obtaining in field measurements of a response function of a calibration filter, wherein said calibration filter is sequentially irradiated by first and second blackbody sources, respectively, wherein said first and second blackbody sources are maintained at temperatures t₁ and t₂, respectively,

3. The method of claim 2, wherein step (a) further comprises the step of obtaining multiple frames of said response function of said calibration filter sequentially irradiated by said first blackbody source at temperature t₁ and said second blackbody source at temperature t₂.

4. The method of claim 1, wherein multiple frames of data are collected at equivalent frame times and ensemble averaged to obtain said response functions in steps (a) and (b).

5. The method of claim 4, wherein step (c) further comprises the step of removing background radiance from said ensemble averaged response functions to produce a spectral transmittance function.

6. The method of claim 1, wherein step (b) comprises the step of obtaining in-field measurements of said response function for said onboard blackbody at temperatures t₁ and t₂, respectively.

7. The method of claim 1, wherein step (c) further comprises the step of normalizing said first derivative function of said spectral transmittance function.

8. The method of claim 1, wherein said step of separating said first derivative function into a plurality of spectral band regions enables the implementation of a full sensitivity to spectral drift, wherein the value of N varies with each of said spectral band regions.

9. The method of claim 1, wherein step (e) comprises the step of determining a sum of the differences between said first derivative function and a reference spectral derivative function from a starting point pixel number to an ending point pixel number for one of said spectral band regions.

10. The method of claim 1, further comprising the steps of:

generating new spectral channel assignments for each pixel of said spectral band region using the spectral magnitude and direction of said spectral drift; and

interpolating values in between.

11. The method of claim 1, further comprising the step of introducing said calibration filter sequentially irradiated by first and second blackbody sources into an optical path of said hyperspectral imaging system using a flip mirror, prior to obtaining in-field measurements of said response function for said calibration filter.

12. The method of claim 5, wherein step (c) comprises the steps of:

determining a spectral difference function, wherein the spectral difference function is the difference between said response function at temperature t₁ and said response function at temperature t₂;

determining a blackbody difference function, wherein the blackbody difference function is the difference between said blackbody source at temperature t₁ and said blackbody source at temperature t₂; and

determining said spectral transmittance function, wherein said spectral transmittance function is the quotient of the spectral difference function and the blackbody difference function.

13. The method of claim 1, wherein the value of N is selected to optimize detection algorithm sensitivity to change while extending a limit of spectral shift magnitude.

14. The method of claim 1, wherein a spectral band per pixel for each spectral band region is defined by an optical geometry, a system focal length, a detector size, and a spectral dispersion rate design of said hyperspectral imaging system.

15. The method of claim 1, wherein the generation of said reference derivative function comprises the steps of:

(1) measuring multiple frames of a reference spectrum of said calibration filter sequentially irradiated by said first and second blackbody sources in a laboratory environment;

(2) measuring multiple frames of a reference spectrum of said first and second blackbody sources in a laboratory environment;

(3) ensemble averaging said reference spectrums from steps (1) and (2);

(4) removing background radiance from said ensemble averaged reference functions to produce a reference spectral transmittance function; and

(5) determining a first derivative of said reference spectral transmittance function.

16. The method of claim 15, wherein step (5) further comprises the step of normalizing said first derivative of said reference spectral transmittance function.

17. The method of claim 1, further comprising the step of generating said look-up table from said first derivative of said reference spectral transmittance function prior to performing step (g).

18. The method of claim 17, wherein said step of generating said lookup table comprises the steps of:

(1) shifting said first derivative of said reference spectral transmittance function by a predetermined shift value in a positive and a negative direction to generate a positive and negative shifted derivative function;

(2) determining the difference between said positive and negative shifted first derivative function and said first derivative of said reference spectral transmittance function to generate pixel shift magnitude values in said positive and negative direction, respectively;

(3) storing said pixel shift magnitude values and the corresponding predetermined shift value in said look-up table; and

(4) repeating steps (1) through (3) using anew predetermined shift value until said spectral band is covered.

19. The method of claim 18, further comprising the step of iteratively repeating steps (1) through (4) for a different spectral band until each of said spectral bands is covered.

20. A computer program product comprising a computer useable medium having computer program logic recorded thereon for enabling a computer to detect spectral drift in a hyperspectral imaging system, said computer program logic comprising:

means for enabling a processor to obtain in-field measurements of a response function for a calibration filter;

means for enabling a processor to obtain in-field measurements of a response function for an onboard blackbody;

means for enabling a processor to determine a spectral transmittance function using said response functions for said calibration filter and said onboard blackbody;

means for enabling a processor to determine a first derivative function of said spectral transmittance function;

means for enabling a processor to separate said first derivative function into a plurality of spectral band regions, each of said spectral band regions having +/−

N pixels on either side of a localized minima;

means for enabling a processor to determine a pixel shift magnitude value for one of said plurality of spectral band regions; and

means for enabling a processor to apply said pixel shift magnitude value to a look-up table to determine a magnitude and direction of said spectral drift for one of said plurality of spectral band regions.

21. The computer program product of claim 20, wherein said means for enabling a processor to obtain in-field measurements of a response function for a calibration filter comprises means for enabling a processor to obtain in-field measurements of a response function for a calibration filter, wherein said calibration filter is sequentially irradiated by first and second blackbody sources, respectively, wherein said first and second blackbody sources are maintained at temperatures t₁ and t₂, respectively,

22. The computer program product of claim 20, wherein said means for enabling a processor to obtain in-field measurements of a response function for a calibration filter further comprises means for enabling a processor to obtain multiple frames of said response function of said calibration filter sequentially irradiated by said first blackbody source at temperature t₁ and said second blackbody source at temperature t₂.

23. The computer program product of claim 20, wherein multiple frames of data are collected at equivalent frame times and ensemble averaged to obtain said response functions for said calibration filter and said onboard blackbody.

24. The computer program product of claim 23, wherein said means for enabling a processor to determine said spectral transmittance function further comprises means for enabling a processor to remove background radiance from said ensemble averaged response functions to produce said spectral transmittance function.

25. The computer program product of claim 20, wherein said means for enabling a processor to obtain in-field measurements of said response function for said onboard blackbody comprises means for enabling a processor to obtain in-field measurements of said response function for said onboard blackbody at temperatures t₁ and t₂, respectively.

26. The computer program product of claim 20, wherein said means for enabling a processor to determine said spectral transmittance function further comprises means for enabling a processor to normalize said first derivative function of said spectral transmittance function.

27. The computer program product of claim 20, wherein said means for enabling a processor to separate said first derivative function into said plurality of spectral band regions enables the implementation of a full sensitivity to spectral drift, wherein the value of N varies with each of said spectral band regions.

28. The computer program product of claim 20, wherein said means for enabling a processor to separate said first derivative function into said plurality of spectral band regions comprises means for enabling a processor to determine a sum of the differences between said first derivative function and a reference spectral derivative function from a starting point pixel number to an ending point pixel number for one of said spectral band regions.

29. The computer program product of claim 20, wherein said control logic further comprises:

means for enabling a processor to generate new spectral channel assignments for each pixel of said spectral band region using the spectral magnitude and direction of said spectral drift; and

means for enabling a processor to interpolate values in between.

30. The computer program product of claim 20, wherein said control logic further comprises means for enabling a processor to introduce said calibration filter sequentially irradiated by first and second blackbody sources into an optical path of said hyperspectral imaging system using a flip mirror, prior to obtaining in-field measurements of said response function for said calibration filter.

31. The computer program product of claim 24, wherein said wherein said means for enabling a processor to determine said spectral transmittance function comprises:

means for enabling a processor to determine a spectral difference function, wherein the spectral difference function is the difference between said response function at temperature t₁ and said response function at temperature t₂;

means for enabling a processor to determine a blackbody difference function, wherein the blackbody difference function is the difference between said blackbody source at temperature t₁ and said blackbody source at temperature t₂; and

means for enabling a processor to determine said spectral transmittance function, wherein said spectral transmittance function is the quotient of the spectral difference function and the blackbody difference function.

32. The computer program product of claim 20, wherein the value of N is selected to optimize detection algorithm sensitivity to change while extending a limit of spectral shift magnitude.

33. The computer program product of claim 20, wherein a spectral band per pixel for each spectral band region is defined by an optical geometry, a system focal length, a detector size, and a spectral dispersion rate design of said hyperspectral imaging system.

34. The computer program product of claim 20, wherein the generation of said reference derivative function comprises:

means for enabling a processor to measure multiple frames of a reference spectrum of said calibration filter sequentially irradiated by said first and second blackbody sources in a laboratory environment;

means for enabling a processor to measure multiple frames of a reference spectrum of said first and second blackbody sources in a laboratory environment;

means for enabling a processor to ensemble average said reference spectrums from said calibration filter and said first and second blackbody sources;

means for enabling a processor to remove background radiance from said ensemble averaged reference functions to produce a reference spectral transmittance function; and

means for enabling a processor to determine a first derivative of said reference spectral transmittance function.

35. The computer program product of claim 34, wherein said means for enabling a processor to determine a first derivative of said reference spectral transmittance function further comprises means for enabling a processor to normalize said first derivative of said reference spectral transmittance function.

36. The computer program product of claim 20, wherein said control logic further comprises means for enabling a processor to generate said look-up table from said first derivative of said reference spectral transmittance function.

37. The computer program product of claim 36, wherein said means for enabling a processor to generate said look-up table comprises:

shifting means for enabling a processor to shift said first derivative of said reference spectral transmittance function by a predetermined shift value in a positive and a negative direction to generate a positive and negative shifted derivative function;

determining means for enabling a processor to determine the difference between said positive and negative shifted first derivative function and said first derivative of said reference spectral transmittance function to generate pixel shift magnitude values in said positive and negative direction, respectively;

storing means for enabling a processor to store said pixel shift magnitude values and the corresponding predetermined shift value in said lookup table; and

repeating means for enabling a processor to repeat said shifting means through said storing means using a new predetermined shift value until said spectral band is covered.

38. The computer program product of claim 37, wherein said control logic further comprises means for enabling a processor to iteratively repeat said shifting means through said repeating means for a different spectral band until each of said spectral bands is covered.