Abstract:
A device, for imaging a scene, includes a detector of the radiation that includes a plurality of detector elements, a circularly variable filter, a mechanism for rotating the filter perpendicular to the optical path of the radiation from the scene to the detector, and a data capture apparatus. All the detector elements are repeatedly interrogated by as a group as the filter rotates, to acquire images of the scene, each of which includes a plurality of image portions in respective spectral bands of the filter. The image portions are assembled to form processed images, each of which depicts the scene in a single respective spectral band.

Description:
This is a continuation-in-part of U.S. patent application Ser. No. 12/853,319, filed Aug. 10, 2010, which is a continuation-in-part of U.S. Provisional Patent Application No. 61/298,569, filed Jan. 27, 2010. This is also a continuation-in-part of U.S. Provisional Patent Application No. 61/487,312, filed May 18, 2011. 
    
    
     FIELD AND BACKGROUND OF THE INVENTION 
     The present invention relates to the detection and imaging of infrared radiation and, more particularly, to a device, for detecting and imaging infrared radiation, that facilitates the alternation among several uncooled filters in conjunction with a cooled detector of the infrared radiation. 
     It is well known in the art of thermal imaging infrared sensors based on cooled detector arrays that in order not to flood the detector with unwanted spurious self-emission from the environment two design elements must be present in the system: i) the collecting optics (lenses or mirrors, filters and windows) must be made of non-absorbing infrared transmitting materials in the wavelength range of sensitivity of the detector (so as not to emit appreciable amounts of infrared radiation introducing noise and masking the radiation to be detected), and ii) the entrance pupil of the collecting optics must be imaged on a cold shield aperture present in the cryogenically cooled space inside the detector Dewar, again in order to avoid radiation from the environment to introduce noise and spurious signals. These design rules are necessary because the optical elements, the optics housing of the system as well as the environment emit a large amount of radiation in the infrared range which in general masks the radiation to be detected and originating in the scene to be analyzed. However in many cases and situations, in addition to the imaging optics and windows, there is the need to use a number of spectral filters placed alternately on the optical train in the sensor system, in order to detect and identify and recognize different sources placed in the field of view of the system. These filters may be narrow-band, wide-band, cut-on, cut-off or otherwise spectrally limiting the incoming radiation from the scene, so that these objects can be detected and identified based on their spectral characteristics. 
     As a result, since a spectral filter may be a source of self-emitted infrared radiation in its own right and may reflect environment radiation into the detector if simply placed in the collection optics train, the common knowledge and practiced art is to place the filter inside the Dewar so as to be cooled to cryogenic temperatures: this insures minimizing the self-emission of the filter and preventing the filter from introducing spurious radiation into the detector. The main disadvantage of this filter cooling method is that once the filter is built into the Dewar it cannot be exchanged for a different one, preventing the possibility of acquiring different successive images of the scene to be analyzed through different narrow wavelengths or through different spectral ranges so that the spectral capability of the system is very limited. 
     The purpose of the present invention is to provide infrared sensor systems with the advantages of the prior art systems that use cooled detectors and a cooled filter but with the significant advantages of: i) enhanced spectral capability by being able to use a succession of spectral filters or a continuously variable filter (CVF) or a different type of filter plurality, ii) avoidance of cooling the filters, which results in a simpler and less expensive system. 
     As it is taught in U.S. Pat. No. 5,434,413 to Kennedy, optical filtering in prior art systems based on cooled photon array detectors can be done for example in the following two ways: i) by placing the filter in direct contact with the cooled detector (see Kennedy FIGS. 1b and 1d) so that the filter itself is cooled and its self-emission is very small, and as a consequence its contribution to signal and background noise is minimized; ii) by placing a bandpass filter coating on the vacuum window (see Kennedy FIG. 2), this window being constructed of a non-absorbing material (see Kennedy, end of column 3): the fact that the window is made of non-absorbing material insures here too that the self-emission of the window and as a consequence its contribution to background noise is minimized even if the window is not cooled. In both configurations of the prior art of Kennedy the filter is constructed as a physical part of the vacuum vessel or Dewar, either inside the vessel or being coated or attached on its window. Both these configurations have the following disadvantages (besides the ones mentioned in that patent for the former configuration). 
     A) These configurations do not allow the use of more than one filter in the system in succession for image detection in more than one spectral range or more than one wavelength (this being the spectral range or the coating of Kennedy FIGS. 1d and 2): in this case, for example, when more than one narrow band signal is needed from each pixel of the image to be measured the filters must be used outside the Dewar on the optical train of the telescope and therefore in general, absent the special innovative improvements of the present invention as described below, the filters will have to be enclosed in an additional vacuum vessel and be cooled in order to avoid their own self-emission. 
     B) Even with this additional cooling of the filters, reflection of background radiation towards the detector in the unwanted noise contributing spectral range cannot in general be avoided. 
     C) The filter configuration inside the Dewar of Kennedy FIGS. 1b and 1d usually requires special work from the detector manufacturers because the filter, being application dependent, is not standard and as a consequence a very high price is paid for the Dewar and detector construction. 
     U.S. Pat. No. 3,770,958 to Krakow teaches the use of a single filter and the use of a series of interchangeable non-emitting uncooled filters placed in front of the Dewar window in a system using a single or multiple stacked detectors (not an imaging array). It is not obvious that such arrangement can be easily extended to the case of imaging array detectors. In fact, in the case of the single filter often there is not enough physical space in front of the window for the filter to be close enough to the Dewar window so that the edge of the array will not receive spurious radiation from the surroundings. The case of a rotating multiple filter wheel in that patent requires a lens to be placed inside the Dewar to be cooled: this is a very expensive and cumbersome proposition. 
     U.S. Pat. No. 5,408,100 to Gallivan teaches an uncooled non-emitting filter that is a multilayer coating, on the last spherical concave surface of a lens in the optical system, whose radius of curvature is equal to the distance of the surface to the detector. This arrangement produces in general an unwanted ghost image of the array pixels superimposed on the desired image provided by the system due to the fact that the pixels and the surface separating them usually have different reflectivity. 
     It would be highly advantageous to be able to use more than one filter in the same system for comparison of signals from different spectral ranges and to use a standard infrared cooled-array-camera-based sensor system without an expensive and cumbersome cooling system needed for any of these filters or lenses and with minimal loss of signal to noise ratio or dynamic range in spite of the filters not being cooled. 
     SUMMARY OF THE INVENTION 
     According to the present invention there is provided a device for imaging a scene, including: (a) a detector, of radiation from the scene, that includes a plurality of detector elements; (b) a circularly variable filter; (c) a mechanism for rotating the circularly variable filter substantially perpendicular to an optical path of the radiation from the scene to the detector; and (d) a data capture apparatus for: (i) repeatedly interrogating all the detector elements as a group while the mechanism rotates the circularly variable filter, thereby acquiring a plurality of acquired images of the scene, each acquired image including a plurality of image portions, with each image portion being acquired in a respective spectral band of the circularly variable filter, and (ii) assembling the image portions to form a plurality of processed images of the scene with each processed image depicting the scene in a single respective spectral band of the circularly variable filter. 
     According to the present invention there is provided a method of imaging a scene, including: (a) focusing radiation from the scene onto a detector that includes a plurality of detector elements; (b) rotating a circularly variable filter substantially perpendicular to an optical path of the radiation from the scene to the detector; (c) synchronous with the rotating, repeatedly interrogating all the detector elements as a group, thereby acquiring a plurality of acquired images of the scene, each acquired image including a plurality of image portions, with each image portion being acquired in a respective spectral band of the circularly variable filter, and (d) assembling the image portions to form a plurality of processed images of the scene with each processed image depicting the scene in a single respective spectral band of the circularly variable filter. 
     According to the present invention there is provided a device for imaging infrared radiation from a scene, including: (a) a detector of the infrared radiation; (b) an enclosure, for keeping the detector at an operating temperature thereof, and including a window that is transparent to the infrared radiation; (c) an optical system, outside of the enclosure, for focusing the infrared radiation through the window onto the detector; (d) a filter having a passband; (e) a mechanism for positioning the filter substantially at an intermediate focal plane of the optical system; and (f) an illuminator for illuminating the scene with infrared radiation in the passband of the filter. 
     A basic embodiment, of a device for imaging a scene, include a detector of radiation from the scene, a circularly variable filter, a mechanism for rotating the filter substantially perpendicular to the optical path of the radiation from the scene to the detector, and a data capture apparatus. The detector includes a plurality of detector elements. The data capture apparatus repeatedly interrogates all of the detector elements as a group while the rotation mechanism rotates the filter, thereby acquiring a plurality of acquired images of the scene. Each acquired image includes a plurality of image portions, each of which is acquired in a respective spectral band of the filter. Then the data capture apparatus assembles the image portion to form a plurality of processed images of the scene. Each processed image depicts the scene in a single respective one of the spectral bands of the filter. Controller  64  of  FIG. 8  below is an example of such a data capture apparatus. 
     Preferably, the device also includes an optical system for focusing the radiation on the detector. The rotation mechanism rotates the filter substantially in an intermediate focal plane of the optical system. More preferably, the radiation includes infrared radiation, and the device also includes an enclosure for keeping the detector at an operating temperature thereof. The enclosure includes a window that is transparent to the infrared radiation. The optical system focuses the infrared radiation through the window onto the detector. Most preferably, the device also includes one or more baffles for shielding the detector from stray radiation. 
     Also more preferably, the optical system is telecentric, with respect to an image space of the optical system, at the intermediate focal plane. 
     In a corresponding method of imaging a scene, radiation from the scene is focused onto a detector that includes a plurality of detector elements. A circularly variable filter is rotated substantially perpendicular to the optical path of the radiation from the scene to the detector. Synchronously with the rotation of the filter, all the detector elements are repeatedly interrogated as a group to acquire a plurality of acquired images of the scene. Each acquired image includes a plurality of image portions. Each image portion is acquired in a respective spectral band of the filter. The image portions are assembled to form a plurality of processed images of the scene, with each processed image depicting the scene in a single respective spectral band of the filter. 
     Dombrowski et al., in U.S. Pat. No. 5,424,543, teach a device and method for using a circularly variable filter to acquire similar “monochromatic” images in the visible portion of the spectrum in real time, by gating their detector to acquire the images synchronously with the rotation of the filter. In the present invention, the acquired images are multi-chromatic, and are disassembled and reassembled to provide the final “monochromatic” images. The present invention is intended primarily for use in the min-infrared portion of the electromagnetic spectrum. Presently known detectors for that portion of the electromagnetic spectrum are not fast enough to acquire images in real time, as in the Dombrowski et al. patent, but the present invention enables relatively fast acquisition, albeit not in real time, of multispectral or hyperspectral images, in a portion of the electromagnetic spectrum that is not accessible to the device and method of the Dombrowski et al. patent. 
     A basic embodiment, of a device for imaging infrared radiation from a scene, includes a detector of the infrared radiation, an enclosure, an optical system outside the enclosure, a passband filter, a mechanism for positioning the filter at or near an intermediate focal plane of the optical system, and an illuminator. The enclosure is for keeping the detector at its operating temperature, which normally is lower than both the ambient temperature of the environment of the device and the temperature of the scene. For example, if the detector is a photon detector, the detector must be kept at cryogenic temperatures in order to work. The enclosure includes a window that is transparent to the infrared radiation. The optical system is for focusing the infrared radiation through the window onto the detector. The illuminator is for illuminating the scene with infrared radiation in the filter&#39;s passband. 
     Preferably, the device includes a plurality of such filters, with each filter having a different respective passband. The positioning mechanism alternately and reversibly positions each filter at the intermediate focal plane. When each filter is so positioned at the intermediate focal plane, the illuminator is used to illuminate the scene with infrared radiation whose wavelengths are confined to the filter&#39;s passband. 
    
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
       Various embodiments are herein described, by way of example only, with reference to the accompanying drawings, wherein: 
         FIG. 1  shows a first embodiment of a device of the present invention; 
         FIG. 2  shows a filter mounted on a holder and inserted in a bracket at the intermediate focal plane of the device of  FIG. 1 ; 
         FIG. 3  shows a filter wheel for use in conjunction with the device of  FIG. 1 ; 
         FIG. 4  shows a variant of the device of  FIG. 1  that includes a baffle for blocking stray radiation; 
         FIG. 5  shows a telecentric variant of the device of  FIG. 1 ; 
         FIG. 6  shows a second embodiment of a device of the present invention; 
         FIGS. 7 and 8  illustrate the use of the device of  FIG. 1  with a circularly variable filter; 
         FIG. 9  illustrates the use of the device of  FIG. 1  along with an illuminator for illuminating the imaged scene. 
     
    
    
     DESCRIPTION OF THE PREFERRED EMBODIMENTS 
     The principles and operation of a device for detecting and imaging infrared radiation according to the present invention may be better understood with reference to the drawings and the accompanying description. 
     The present invention is specifically directed to a new way of successively filtering spectral ranges of detected infrared radiation that avoids cooling the filters themselves, and at the same time does not lose appreciably the low noise advantage given by this cooling and adds the advantage of easily scanning through different wavelengths of filtering in a compact and less expensive fashion than in the prior art. 
     The traditional stand-off detection and identification of objects exhibiting narrow spectral absorption features in the infrared region of the spectrum are done by instrumentation which is capable of sensing either spectral radiation intensity as function of wavelength in a wide spectral range, or material specific radiation selected by a specific spectral filter in a narrow characteristic region of the spectrum appropriate for that material. This is so because the functional shape of this wavelength dependent radiation intensity is directly related to the specific spectral characteristics of the material and to its chemical composition and can be used for its detection, recognition or identification and imaging. In contrast, an instrument without a spectral capability, such as an infrared radiometric camera, measuring or displaying only the integral of the radiation emitted by a scene within a whole spectral range, cannot distinguish between different compositions or types of materials, because in this case the signal is only correlated to the temperature and average emissivity of the material in question, and does not yield material-specific information. 
     Therefore, it would be desirable to have an infrared optical detection system with an infrared cooled detector array which is capable of imaging infrared radiation emitted by objects to be identified and located by detecting and comparing the objects&#39; spectral features or emissions in different spectral narrow wavelength bands in a relatively simple and inexpensive opto-mechanical configuration. 
     Many types of radiation measuring instrumentation have been developed and sold for this purpose for many years, with partial or full spectral capability. Some types of instrumentation are quite complex in their design and manufacturing due to the need for means of optically dispersing (by way of prisms, gratings, etc. subsystems) or i handling (by way of an interferometer) the measured radiation interacting with the object to be detected. This fact makes this type of instrument usually large, heavy and expensive. Simpler instrumentation is based on spectrally specific radiation filtering; this requires that the filter be cooled to cryogenic temperatures in case this filtering is done by full or partial absorption of the radiation being filtered and the filter placed in the Dewar right in front of the detector; otherwise the detector may be flooded by a large unspecific signal due to the filter&#39;s own infrared self emission or originated by the environment and reflected by the filter, making it impossible for the sought-after signal to be detected. This need for cooling the filter complicates the design and implementation of the instrument. 
     According to the present invention the detection and imaging of a specific material (such as a gas cloud or terrain in geological analysis or other infrared spectrally active material) from a distance is done with an array-based infrared camera combined with material-specific filtered optics, avoiding the cooling of the filter and at the same time providing either a partial or full spectral capability for single or multiple material identification without losing most of the noise reduction advantage of the filter cooling. The solution is provided by several, elements: i) any filter in the system is designed in such a way that in the wavelength range of sensitivity of the detector the filter barely absorbs any radiation, for minimum self-emission, ii) an optical design of the system that insures that the only spurious radiation reaching the detector in addition to the specifically filtered radiation from the object to be studied is radiation originating from the cooled region of the detector itself or from a cold region within the Dewar, therefore being negligible; this can be achieved, for example, with a non-absorbing filter on a non-absorbing substrate (single or multiple on a rotating filter wheel, or a continuously circular variable spectral filter, so called CVF, or linearly variable spectral filter, so called LVF) placed in or near an intermediate image plane of the collecting optics and combined with relay optics to image the intermediate image plane on the detector array, or with a non-absorbing filter coating on a concave spherical lens surface (also usually combined with additional optics for imaging on the detector array) placed at a distance from the cold shield equal to the radius of curvature of this surface; and iii) a cooled detector-array-based infrared camera: in fact, the self-emission of the array is negligible in this case because it is cooled and therefore it may be used as background to the signals to be detected without appreciably contributing to those signals and to background noise. Reflecting baffles may be necessary to prevent residual stray radiation from reaching the detector. 
     A system of the present invention, for sensing infrared signals in a single or a plurality of specific narrow spectral regions of the infrared spectrum in succession, is designed so that almost all the signal recorded by the detector is only from two possible sources: the object-specific self-emission to be identified in the wavelength range(s) of transmission of the filter or filters (allowing identification), and a very small signal emitted by the cooled detector or cold region within the Dewar as background with no other or almost no other spurious contribution from the environment. 
     Referring now to the drawings,  FIG. 1  shows a first embodiment  10  of a device for imaging a scene  26 , such as a gas cloud, in the infrared region of the electromagnetic spectrum. The imaging itself is done by a photon detector array  20  that is cooled by the conventional method of being mounted on a cold finger  14  inside a Dewar  12 . Cooling is provided by a cryogenic fluid  18  such as liquid nitrogen inside cold finger  14 . Alternatively, cooling is provided by a closed-cycle cooling system such as a Stirling cooler, also to the 77° K temperature of boiling liquid nitrogen. Detector array  20  is insulated thermally from the outside environment of device  10  by the vacuum  16  of Dewar  12 . Detector array  20  is further shielded from stray infrared radiation by a cold shield  22  that is cooled by thermal contact with cold finger  14 . Infrared radiation from scene  26  is focused on detector array  20  through a window  24  by a telescope  28  whose optical components are represented symbolically in  FIG. 1  by lenses  30  and  32 . (Each of “lenses”  30  and  32  actually is a set of one or more lenses that is represented in  FIG. 1  by a single lens.) Window  24  and optical components  30  and  32  are made of materials, such as germanium, zinc sulfide or zinc selenide, that is transparent in the infrared. The surfaces of window  24  and optical components  30  and  32  are coated with antireflection coatings. 
     For clarity of illustration, the image acquisition electronics associated with detector array  20  are not shown in  FIG. 1 . 
     A filter  36 A is positioned in the optical path of telescope  28  at or near an intermediate focal plane  34  of telescope  28  so that all the rays from scene  26  that are focused on detector array  20  by telescope  28  pass through filter  36 A. 
       FIG. 2  shows one way of positioning filter  36 A in the optical path of telescope  28  at intermediate focal plane  34 . Device  10  is provided with a bracket  54  for holding a rectangular holder  52 , in which filter  36 A is mounted, substantially coincident with intermediate focal plane  34 . The positions of lenses  30  and  32  relative to holder  52 , when holder  52  is inserted into bracket  54  with filter  36 A in the optical path of telescope  28  as shown in  FIG. 1 , are shown in  FIG. 2  in phantom. As long as card  52  is mounted inside bracket  54  as shown, filter  36 A is fixed in place in the optical path of telescope  28  at intermediate focal plane  34 . Similar holders, having mounted therein other filters  36 B,  36 C,  36 D, etc., are also provided, so that filter  36 A can be swapped for the other filters, for example for detection of a gas by comparison of images at different wavelengths or for identification of different materials with different spectral features. 
       FIG. 3  shows another way of positioning filter  36 A in the optical path of telescope  28  at intermediate focal plane  34 . In  FIG. 3 , filter  36 A is one of four filters  36 A,  36 B,  36 C and  36 D that are mounted on a filter wheel  38 . Filter wheel  38  is mounted in device  10  substantially coincident with intermediate focal plane  34  and is rotated about its center to position one of filters  36 A,  36 B,  36 C or  36 D, as desired, in the optical path of telescope  28 . The positions of lenses  30  and  32  relative to filter wheel  38 , when filter  36 A is in the optical path of telescope  28  as shown in  FIG. 1 , are shown in  FIG. 3  in phantom. That filter wheel  38  includes only four filters  36  is only for illustrational clarity. Filter wheel  38  may include as many filters as is convenient, for example for detection of a gas by comparison of images at different wavelengths or for identification of different materials with different spectral features. 
     Alternatively, the filter that is positioned in the optical path of telescope  28  at intermediate focal plane  34  is a circular variable filter having a continuously variable transmitted wavelength around its circumference or a linearly variable filter having a continuously variable transmitted wavelength along one of its dimensions perpendicular to the optical path of telescope  28 . 
     All the filters of the preferred embodiments are filters such as interference filters that do not appreciably absorb and emit radiation within the spectral window of sensitivity of detector array  20 . 
       FIG. 4  shows a variant of the embodiment of  FIG. 1  in which a baffle  42  has been added to keep infrared radiation that originates in the environment of device  10  from reaching detector array  20 . The example of such self-emission that is shown in  FIG. 4  is a ray  44  from one of the internal walls  40  of device  10 . Baffle  42  is a highly reflective mirror on the side that faces telescope  28 , and in this example is shaped like the frustum of a cone, with an aperture in its center. A baffle such as baffle  42  that prevents stray radiation from reaching detector array  20  is more important for the detector elements near the edges of detector array  20  than for the detector elements towards the middle of detector array  20 . 
     Alternately or additionally, spurious radiation is prevented from reaching detector array  20  by configuring telescope  28  with optics that are telecentric with respect to the image space of telescope  28  at intermediate focal plane  34  so that the central rays from scene  26  are perpendicular to filter  36 A. Such a telecentric arrangement is equally beneficial for both the detector elements near the edges of detector array  20  and the detector elements towards the middle of detector array  20 . 
       FIG. 5  illustrates such a telecentric variant  10  of embodiment  10 , with two objective lenses  30 A and  308  and two relay lenses  32 A and  32 B in telescope  28 . Rays  70 ,  72  and  74  from the center of a distant scene are focused on the center of detector array  20 . Rays  76 ,  78  and  80  from one side of the scene are focused towards an edge of detector array  20 . The central rays, rays  72  and  78 , are perpendicular to filter  36 A. Such a design guarantees that while all the light from the scene that traverses filter  36 A is focused onto detector array  20  any other light reflected by filter  36 A towards detector array  20  is negligible because that light originates in a cold region, i.e., the region near the detector itself, which region is kept chilled by cryogenic fluid  18  of  FIG. 1 . 
     The baffles of  FIG. 4  and the telecentric arrangement of  FIG. 5  minimize the light that is reflected by filter  36 A towards detector array  20 . Such reflected light is the principal contribution to stray light because filter  36 A, being highly reflective for all wavelengths except the wavelengths for which filter  36 A is highly transmissive, acts as a mirror for those wavelengths and may easily direct a large number of unwanted photons from the environment of device  10  to detector array  20 . The other components in the optical train, such as lenses  30  and  32 , are coated with antireflection coatings for the same purpose. 
       FIG. 6  shows a second embodiment  10 ′ of a device for imaging scene  26 . Embodiment  10 ′ is similar to embodiment  10  except that in telescope  28  lens  32  has been replaced with a set  46  of one or more lenses whose surface  48  closest to detector array  20  is concave towards detector array  20 . Here, the filter is not a separate optical element from the focusing optics of telescope  28  but rather a non-absorbing coating  50  on surface  48 . For clarity of illustration, the thickness of coating  50  is greatly exaggerated in  FIG. 6 . The radius of curvature of surface  48 , and so of coating  50 , is equal to the distance d between surface  48  and the aperture of cold shield  22  along the optical axis of telescope  28 . In this case there is no need for the optics of telescope  28  to include an intermediate focal plane, but the successive detection of the radiation through a plurality of filters is possible only by replacing lens set  46 , or at least by replacing the lens of set  46  closest to detector array  20 , which is a more cumbersome method than the methods used with the embodiments of  FIGS. 1-5 . 
     The advantage of having cold shield  22  being imaged by surface  48  and filter  50  onto cold shield  22  itself, rather than onto detector array  20  as in the device of Gallivan, is that the design of  FIG. 6  maintains the purpose of having a cold region being reflected by surface  48  and filter  50  onto detector array  20  without introducing a spurious ghost pattern onto the image acquired by detector array  20  due to the non-uniform emissivity of the detector plane. 
     Like device  10 , device  10 ′ may optionally include one or more baffles to prevent stray emission from the environment from reaching detector array  20 . 
     Returning to the embodiment of  FIG. 1 ,  FIG. 7  illustrates a most preferred mode of using this embodiment with a circular variable filter at intermediate focal plane  34  to acquire a spectral cube, i.e., a set of images of scene  26  at more-or-less equally spaced wavelengths. Strictly speaking, what is illustrated is a slightly less preferred mode of using the circular variable filter. At any position of the filter, a small number of adjacent spectral bands of light from the scene are focused on respective trapezoidal or triangular regions  21  of detector array  20 . Regions  21  are of approximately equal angular width. (That regions  21  are not of equal angular width is due to the fact that in practice the spectral resolution of a circular variable filter varies with wavelength.) In the illustrated example, there are eleven such regions,  21 A through  21 K. Region  21 A receives light of a first spectral band, region  21 B receives light of a second spectral band, etc. and region  21 K receives light of an eleventh spectral band. Each region  21  of detector array  20  is used to acquire a sub-image of a respective portion of scene  26  in the respective spectral band of that region  21 . Then the circular variable filter is rotated so that region  21 A receives light of the second spectral band, region  21 B receives light of the third spectral band, etc., region  21 J receives light of the eleventh spectral band, and region  21 K receives light of a twelfth spectral band. Again, each region  21  of detector array  20  is used to acquire a sub-image of a respective portion of scene  26  in the respective spectral band of that region  21 . The stepwise or continuous rotation of the circular variable filter and the associated imaging and storage of successive array frames are continued until all or a sufficiently large number of the adjacent spectral bands in the wavelength range of the CVF have been imaged in all regions  21 . If the filter “wraps around”, which is the case if, for example, the filter occupies a full circle or each of two identical filters occupies a half circle, in the acquisition of the last acquired image, when region  21 A receives light of the last spectral band, region  21 B is receiving light of the first spectral band, region  21 C is receiving light of the second spectral band, etc. and region  21 K is receiving light of the tenth spectral band. If the filter does not wrap around, the same full spectral coverage still can be obtained, albeit not as quickly, by a sufficient rotation of the filter. Then all the sub-images that were acquired in the first spectral band are assembled to create an image of the entire scene  26  in the first spectral band, all the sub-images that were acquired in the second spectral band are assembled to create an image of the entire scene  26  in the second spectral band, and so on through the spectral bands past the second spectral band, until finally all the sub-images that were acquired in the last spectral band are assembled to create an image of the entire scene  26  in the last spectral band. 
     In the actual most preferred mode of using a circular variable filter, instead of stepwise rotation of the circular variable filter the circular variable filter is rotated continuously at an angular speed of one region  21  per frame. So, for example, if the angular width of each region  21  corresponds to a two-degree rotation of the circular variable filter, each image is acquired during each such two-degree rotation of the circular variable filter. 
     In a typical configuration of the first embodiment with a circular variable filter, the overall passband of the filter is between 8 microns and 12 microns. The filter resolution is 0.5%, so that there are 100 filter resolution elements in the filter&#39;s 8 to 12 micron passband. The active area of the filter includes two half-rings of 42 millimeter radius, for a length of 132 millimeters per half-ring. Each half-ring spans the 8 to 12 micron passband, so each filter resolution element has an angular size of 1.8 degrees. Correspondingly, the angular size of each region  21  is 1.8 degrees. Detector array  20  has a maximum frame rate of 250 Hz. 
     The steps in the acquisition of a 100-image spectral cube then are as follows. Every four milliseconds, an image is recorded using detector array  20 , while rotating the filter by 1.8 degrees. This combined image recording and filter rotation is repeated 100 times while recording the images in a memory. In this manner, five spectral cubes are acquired every two seconds. 
       FIG. 8  is  FIG. 1  enhanced to illustrate more completely the embodiment of  FIG. 1  configured for this most preferred mode of using a circularly variable filter. Specifically, in  FIG. 8 , filter  36 A has been replaced with a circularly variable filter  60  that is rotated by a motor  62  about an axis  66 . A system controller  64  uses detector array  20  to acquire images of scene  26  and synchronizes the rotation of filter  60  with the acquisition of the images as described above. After acquiring a sufficiently large number of images, system controller  64  dissects and reassembles the acquired images to produce the desired set of “monochromatic” processed images of scene  60 . 
     After all the spectral image data elements have been stored in a computer memory as a “spectral cube”, the stored data can be analyzed in many ways. Just as each element of a two-dimensional image is a “pixel”, so each element of a (three-dimensional) spectral cube is a “voxel”. Each set of voxels associated with a particular image pixel coordinate pair is a spectrum associated with an image pixel of scene  26 . One way to display a summary of a spectral cube is to compare each such spectrum with a set of reference spectra of known materials and to assign each pixel of the image of scene  26  a respective color according to which reference spectrum the pixel&#39;s spectrum most closely resembles. 
       FIG. 9  illustrates a most preferred mode of using a single filter  36 A, or a set of discrete filters such as the set  36 A through  36 D on filter wheel  38  of  FIG. 3 , in conjunction with auxiliary illumination of scene  26 . Specifically,  FIG. 9  includes, in addition to the components illustrated in  FIG. 1 , an illuminator  70  for illuminating scene  26  with infrared light  72  as described below. 
     In some security (and other) applications the spatial distribution of certain chemical materials, such as drugs, explosives, etc. is detected on clothes, suitcases and other objects by illuminating the object with incoherent or laser light in the thermal infrared region between about seven to fourteen microns or sub-bands thereof and by imaging the backscattered light with an infrared camera sensitive in the same wavelength range. The illumination (coherent or not) may be of a single wavelength or it may be tunable in a continuous range or in a number of discrete wavelengths in the range. 
     In general, images of the same object illuminated at different wavelengths are compared mathematically and the detection, identification and spatial distribution of such chemicals are obtained by using advanced calibration and detection algorithms applied to those images. These algorithms take advantage of the different spectral signatures of these sought for chemicals with respect to common materials such as plastics, wood, metals, paints, clothing materials like cotton, wool etc. 
     Typical distances reported in the literature at which this method works (for example see “Imaging standoff detection of explosives using widely tunable mid-infrared quantum cascade lasers” by Frank Fuchs et al., Optical Engineering 49 (11) p. 111127 (2010)) are several centimeters to several meters. 
     It is well known that many parameters of the measurement conditions may affect the detection accuracy (sensitivity and specificity) and the longest distance at which the method is useful. These parameters include the laser average power (if a laser is used for illumination), the spectral reflection characteristics of the object and the chemical, the speckle noise, the camera noise, the background noise, etc. 
     The embodiment of  FIG. 9  is useful in the case in which the dominant limiting factor of the chemicals&#39; detection is the background signal and noise due to the self-emission of the object being studied and of the background self-emission reflected by the object being studied into the imaging camera. This radiation is of blackbody type at room temperature and therefore it does not carry any specific information on the chemical to be detected: as a result, it represents an unwanted contribution to the camera signals. The intensity of this radiation limits the dynamic range of the measurement, while the shot noise due to the self-emitted photons limits the signal to noise ratio of the recorded signals, affecting the discrimination limits of the signatures in question. 
     Configuring the imaging camera as illustrated in  FIG. 9  significantly improves the results and the detection limits of the system itself with respect to the case in which a simple thermal camera is used as the imaging device. In the case that wide band or filtered incoherent illumination or a laser is used at a single wavelength the embodiment of  FIG. 9  yields these improved results with one single filter  36 A at a wavelength matched to the filtered source or the laser while recording the object image. In the case that the laser or filtered incoherent wide band source is tuned to a sequence of wavelengths, filter wheel  38  (or, equivalently, a continuously variable filter that is large enough, compared to the image focused on detector array  20 , that there is only one region  21 ) is the relevant solution. In this case wavelength matching and synchronization must be added to system  10  to rotate filter wheel  38  so that filter wheel  38  is positioned on the optical train at the same wavelength as the instantaneous wavelength of the filtered source or tuned laser. The advantage provided by the “Cold Filter” idea, which consists in not being cryogenically cooled and at the same time not contributing self-emission to the signals, is also important. 
     By limiting the imaging of the object and background self-emission (superimposed on the backscattered radiation of the source) to the narrow bandpass of the instantaneous single filter  36  this unwanted signal is reduced by a large factor. This factor depends on the value of the filter bandwidth and on the wavelength range of sensitivity of detector  20 . For example, at 25° C. the Planck function radiance integrated in the 7 to 12 micron range is:
 
 W   25C,7-12 =2.2×10 −2  Watts/(cm 2 ·sr),  (1)
 
whereas the integral of the Planck function radiance in a range of width 0.044 microns around 7.4 microns is
 
 W   25C,7.4 =2.4×10 −4  Watts/(cm 2 ·sr).  (2)
 
(2) is a factor of about 100 less than (1). Since filter  36 , due to its own design, hardly contributes any self-emission itself in the wavelength range in consideration, this is enough to prove the improvement brought about by this method.
 
     While the invention has been described with respect to a limited number of embodiments, it will be appreciated that many variations, modifications and other applications of the invention may be made. Therefore, the claimed invention as recited in the claims that follow is not limited to the embodiments described herein.