USH1354H - Optical data transducer - Google Patents

Optical data transducer Download PDF

Info

Publication number
USH1354H
USH1354H US07/772,199 US77219991A USH1354H US H1354 H USH1354 H US H1354H US 77219991 A US77219991 A US 77219991A US H1354 H USH1354 H US H1354H
Authority
US
United States
Prior art keywords
dewar
array
spatial light
light modulator
optical
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US07/772,199
Inventor
Otto R. Martinez
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
US Air Force
Original Assignee
US Air Force
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by US Air Force filed Critical US Air Force
Priority to US07/772,199 priority Critical patent/USH1354H/en
Application granted granted Critical
Publication of USH1354H publication Critical patent/USH1354H/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01JMEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
    • G01J5/00Radiation pyrometry, e.g. infrared or optical thermometry
    • G01J5/10Radiation pyrometry, e.g. infrared or optical thermometry using electric radiation detectors
    • G01J5/28Radiation pyrometry, e.g. infrared or optical thermometry using electric radiation detectors using photoemissive or photovoltaic cells
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01JMEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
    • G01J5/00Radiation pyrometry, e.g. infrared or optical thermometry
    • G01J5/02Constructional details
    • G01J5/06Arrangements for eliminating effects of disturbing radiation; Arrangements for compensating changes in sensitivity
    • G01J5/061Arrangements for eliminating effects of disturbing radiation; Arrangements for compensating changes in sensitivity by controlling the temperature of the apparatus or parts thereof, e.g. using cooling means or thermostats

Definitions

  • the present invention relates generally to optical data transducer devices, and more particularly to an improved cryogenic dewar and optical data transducer system configured to efficiently extract information from within the dewar using a spatially modulated low power laser beam.
  • Sensitive infrared focal plane arrays normally must be disposed within a cryogenic dewar for operation at low temperature.
  • high data rates are necessary in order to efficiently extract information from the dewar to an externally located detection system.
  • high data extraction rates carry a corresponding penalty of a need for a large number of electrical leads from the dewar. As a result, severe vacuum loss and heat leak problems arise.
  • the invention solves or substantially reduces in critical importance problems with prior art systems as just described by providing a cryogenic dewar and optical transducer system comprising an optical spatial light modulator in conjunction with a collimated laser probe beam and an IRFPA for efficient extraction of information from the IRFPA using a maximum of four electrical leads (system clock, ground, and two power leads) to the dewar.
  • the invention has substantial application in systems using cryogenically cooled infrared detectors, such as infrared search and track sets, guidance systems and imaging systems.
  • FIG. 1 is a schematic perspective view of a conventional dewar system for cooling a sensitive infrared focal plane array
  • FIG. 4 is a schematic of a basic transducer layout within a dewar for illustrating the general operation of the invention
  • FIG. 5 is a schematic of an alternative transducer system within a dewar using a two dimensional infrared focal plane array and a one dimensional spatial light modulator;
  • FIG. 6 is a schematic of another transducer system within a dewar using a one dimensional infrared focal plane array and a two dimensional spatial light modulator according to a further aspect of the invention.
  • FIG. 7 is a schematic of yet another transducer system within a dewar using a one dimensional infrared focal plane array and a one dimensional modulator.
  • FIG. 1 shows a schematically a perspective view of a conventional dewar system 10 for cooling a sensitive infrared focal plane array 11.
  • array 11 is immersed in a cryogen 13 such as liquid argon, liquid nitrogen or liquid helium within a heat conduction to array 11.
  • Array 11 normally operates within a dewar cooled below about -200° C.
  • Data, control and power lines 20-23 interconnect array 11 and electronics (not shown) external of container 15 and may be disposed within container 15 or etched on a wall thereof.
  • an optical window 47 is defined in a wall of dewar 33 through which data may be extracted from system 30.
  • a reflective spatial light modulator 49 (such as a deformable mirror array) is disposed on the cold finger of dewar 33 confronting window 47 as suggested in FIG. 2.
  • Modulator 49 is operatively connected through amplifier bank 51 to array 31 via bus 53 comprising any suitable number of electrical leads.
  • FIG. 3 schematically illustrates in section typical construction of a micro mirror segment 55 of which the deformable mirror array is comprised.
  • Each mirror segment 55 is about 6 ⁇ 10 -7 to 4 ⁇ 10 -5 square inch in area, and comprises a substrate 56 of p or n type semiconductor material, such as silicon or gallium arsenide.
  • a driving electrode 57 of aluminum, gold or silver is deposited on substrate 56 and is operatively connected to an electrical lead (not shown) included in bus 53.
  • Mirror 58 supporting a mirrored surface 59 is deposited or otherwise disposed on substrate 56 over electrode 57 as suggested in FIG. 3.
  • Mirrored surface 59 may comprise aluminum, silver or other suitable metallic.
  • Each mirror 58 of each mirror segment 55 may be fabricated by microscopic machine construction techniques or other method occurring to one skilled in the applicable art.
  • Each mirror 58 is structured as a cantilevered plate which is deformed to a degree corresponding to the amount of electrical current applied to energize the corresponding electrode 57.
  • a laser probe beam 61 is projected from a source 62 thereof and may be collimated by collimating lens 63 (FIG. 2).
  • Probe beam 61 is incident onto modulator 49 comprising such as an array of mirror segments 55.
  • Each mirror segment 55 in the array cooperates with other segments 55 to shift the phase and/or amplitude of beam 61 in proportion to the current applied to the segment.
  • FIG. 5 illustrates an alternative transducer system 90 within dewar 91 using two dimensional infrared focal plane array 93 and one dimensional modulator 95 for two dimensional to one dimensional data transfer according to an aspect of the invention.
  • counter 101 is initially reset to mark the beginning of a frame period and increases in value at the occurrence of each following cycle of the system clock.
  • the value impressed on counter 101 is decoded by multiplexer 104 which enables a single line for data from a row or column (depending on read-out structure) to be applied to a row of electrodes within array 93.
  • the set of column or row data is then presented to amplifier bank 97 which amplifies the signals for transmission over bus 98 to linear modulator 95.
  • Modulator 95 is then illuminated by a low power laser (61 of FIG 2), the reflected beam (beam 61' of FIG. 2) being encoded with an image of a single row of array 93 and directed a detector system.
  • the value on counter 101 is then increased on the next cycle of the system clock to enable the next row or column for transfer to modulator 95.
  • the process is then repeated for the remaining rows during the frame period until the entire image from array 93 is transferred to the digital or optical processor external of dewar 91.
  • Counter 101 is then reset to the first row of array 93 and the sequence repeated for each following frame period.
  • FIG. 6 illustrates yet another transducer system 110 within dewar 111 using one dimensional infrared focal plane array 113 and two dimensional modulator 115 for one dimensional to two dimensional data transfer according to yet another aspect of the invention.
  • No counter is needed for array 113 since but a single line of information exists therein.
  • the clock cycle may be used to cycle array 113.
  • Counter 121 records the image gathered by array 113 on modulator 115.
  • the clock signal activates transfer of data to the row electrodes of array 113 and counter 121 of modulator 115 is set to a value corresponding to the first row of the image to be scanned.
  • the row data from array 113 is then transferred to the amplifier bank 117 for transmission to modulator 115 and applied to the row of modulator 115 corresponding to the row in the image being scanned.
  • the value on counter 121 is then increased to coincide with the next row of imagery from (linear) array 113, and the foregoing process is repeated until modulator 115 contains the entire image scanned by array 113.
  • Modulator 115 is then illuminated by a low power laser as above to encode the reflected beam with the image stored in modulator 115 and to direct the encoded beam to a detector, which marks the end of a frame period.
  • Counter 121 is then reset to the top row of modulator 115 and the sequence repeated for each following frame period.
  • FIG. 7 illustrates another transducer system 130 within dewar 131 using one dimensional infrared focal plane array 133 and one dimensional modulator 135 for one dimensional to one dimensional data transfer according to the invention.
  • No counter is needed in system 130 since there is only a single line of information.
  • the clock cycle is used to cycle array 133 and modulator 135.
  • the clock signal activates data transfer to the row electrodes of array 133.
  • the row data is amplified by amplifier bank 137 and transmitted to modulator 135.
  • Modulator 135 is then illuminated by a low power laser as above to encode the reflected beam with the image stored in modulator 135 and to direct the encoded beam to a detector.
  • the invention therefore provides an improved cryogenic dewar and optical data transducer system configured with a minimum number of electrical input leads and wherein data is efficiently extracted from the dewar optically and in parallel allowing high frame rates without corruption of the data during transmission. It is understood that modifications to the invention may be made as might occur to one with skill in the field of the invention within the scope of the appended claims. All embodiments contemplated hereunder which achieve the objects of the invention have therefore not been shown in complete detail. Other embodiments may be developed without departing from the spirit of the invention or from the scope of the appended claims.

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Spectroscopy & Molecular Physics (AREA)
  • Photometry And Measurement Of Optical Pulse Characteristics (AREA)
  • Transforming Light Signals Into Electric Signals (AREA)

Abstract

An optical data transducer system is described which comprises a cryogenic dewar for containing an infrared focal plane array at low temperature and an optical spatial light modulator, collimated laser beam and associated optical train and detector for efficient extraction of information from the array.

Description

RIGHTS OF THE GOVERNMENT
The invention described herein may be manufactured and used by or for the Government of the United States for all governmental purposes without the payment of any royalty.
BACKGROUND OF THE INVENTION
The present invention relates generally to optical data transducer devices, and more particularly to an improved cryogenic dewar and optical data transducer system configured to efficiently extract information from within the dewar using a spatially modulated low power laser beam.
Sensitive infrared focal plane arrays (IRFPA) normally must be disposed within a cryogenic dewar for operation at low temperature. In the operation of an IRFPA, high data rates are necessary in order to efficiently extract information from the dewar to an externally located detection system. In conventional systems, high data extraction rates carry a corresponding penalty of a need for a large number of electrical leads from the dewar. As a result, severe vacuum loss and heat leak problems arise.
The invention solves or substantially reduces in critical importance problems with prior art systems as just described by providing a cryogenic dewar and optical transducer system comprising an optical spatial light modulator in conjunction with a collimated laser probe beam and an IRFPA for efficient extraction of information from the IRFPA using a maximum of four electrical leads (system clock, ground, and two power leads) to the dewar. The invention has substantial application in systems using cryogenically cooled infrared detectors, such as infrared search and track sets, guidance systems and imaging systems.
It is therefore a principal object of the invention to provide an improved optical transducer system.
It is another object of the invention to provide a cryogenic dewar improved with an optical data transducer to extract information from the dewar.
It is yet another object of the invention to provide a cryogenic dewar and optical spatial light modulator and collimated laser beam system for efficient extraction of information from a cryogenically cooled IRFPA using a minimum of electrical leads.
It is yet another object of the invention to provide a combined reflective spatial light modulator and IRFPA.
These and other objects of the invention will become apparent as a detailed description of representative embodiments proceeds.
SUMMARY OF THE INVENTION
In accordance with the foregoing principles and objects of the invention, an optical data transducer system is described which comprises a cryogenic dewar for containing an infrared focal plane array at low temperature and an optical spatial light modulator, collimated laser beam and associated optical train and detector for efficient extraction of information from the array.
DESCRIPTION OF THE DRAWINGS
The invention will be more clearly understood from the following detailed description of representative embodiments thereof read in conjunction with the accompanying drawings wherein:
FIG. 1 is a schematic perspective view of a conventional dewar system for cooling a sensitive infrared focal plane array;
FIG. 2 is a schematic layout of an optical transducer system and modified dewar according to the invention including associated external optics and electronics;
FIG. 3 is a schematic cross-sectional view of a micro mirror which the deformable mirror array of the invention may comprise;
FIG. 4 is a schematic of a basic transducer layout within a dewar for illustrating the general operation of the invention;
FIG. 5 is a schematic of an alternative transducer system within a dewar using a two dimensional infrared focal plane array and a one dimensional spatial light modulator;
FIG. 6 is a schematic of another transducer system within a dewar using a one dimensional infrared focal plane array and a two dimensional spatial light modulator according to a further aspect of the invention; and
FIG. 7 is a schematic of yet another transducer system within a dewar using a one dimensional infrared focal plane array and a one dimensional modulator.
DETAILED DESCRIPTION
Referring now to the drawings, FIG. 1 shows a schematically a perspective view of a conventional dewar system 10 for cooling a sensitive infrared focal plane array 11. In conventional designs as represented by system 10, array 11 is immersed in a cryogen 13 such as liquid argon, liquid nitrogen or liquid helium within a heat conduction to array 11. Array 11 normally operates within a dewar cooled below about -200° C. Data, control and power lines 20-23 interconnect array 11 and electronics (not shown) external of container 15 and may be disposed within container 15 or etched on a wall thereof. In the operation of array 11, high data rates may be necessary to extract information from array 11 to a data processor external of system 10, and may dictate the need for an undesirably great number of electrical leads (well in excess of the four suggested in FIG. 1) for data extraction purposes. The greater number of leads may result in substantial vacuum loss and heat leak problems for system 10.
Referring now to FIG. 2, shown therein is a schematic layout of an optical transducer system 30 constructed according to the invention, including associated external optics and electronics. Infrared focal plane array 31 may, in substantially conventional fashion, be mounted within dewar 33 near an optical window 35 through a wall of dewar 33 for receiving an external signal in the form of infrared radiation 37. No more than four electronic leads 39-42 interconnect array 31 and input electronics 45 disposed external of dewar 33, providing input for a system clock, power (-V and +V) and ground.
In accordance with a principal feature of the invention, an optical window 47 is defined in a wall of dewar 33 through which data may be extracted from system 30. A reflective spatial light modulator 49 (such as a deformable mirror array) is disposed on the cold finger of dewar 33 confronting window 47 as suggested in FIG. 2. Modulator 49 is operatively connected through amplifier bank 51 to array 31 via bus 53 comprising any suitable number of electrical leads.
A deformable mirror array may be preferred for use in system 30 because spatial light modulators based on liquid crystals may be inoperative at the cryogenic temperatures contemplated for operation of system 30. FIG. 3 schematically illustrates in section typical construction of a micro mirror segment 55 of which the deformable mirror array is comprised. Each mirror segment 55 is about 6×10-7 to 4×10-5 square inch in area, and comprises a substrate 56 of p or n type semiconductor material, such as silicon or gallium arsenide. A driving electrode 57 of aluminum, gold or silver is deposited on substrate 56 and is operatively connected to an electrical lead (not shown) included in bus 53. Mirror 58 supporting a mirrored surface 59 is deposited or otherwise disposed on substrate 56 over electrode 57 as suggested in FIG. 3. Mirrored surface 59 may comprise aluminum, silver or other suitable metallic. Each mirror 58 of each mirror segment 55 may be fabricated by microscopic machine construction techniques or other method occurring to one skilled in the applicable art. Each mirror 58 is structured as a cantilevered plate which is deformed to a degree corresponding to the amount of electrical current applied to energize the corresponding electrode 57. A laser probe beam 61 is projected from a source 62 thereof and may be collimated by collimating lens 63 (FIG. 2). Probe beam 61 is incident onto modulator 49 comprising such as an array of mirror segments 55. Each mirror segment 55 in the array cooperates with other segments 55 to shift the phase and/or amplitude of beam 61 in proportion to the current applied to the segment. Beam 61 is therefore modulated by signals from array 31 to modulator 49 (represented by the array of mirror segments 55). An optical train 65 including any required number of optical elements such as mirror 66 and beamsplitter 67 direct the incident beam 61 to modulator 49 and direct the modulated beam 61' to a detector system such as charged couple device (CCD) photodiode array 69 and display 70, digital processor or other detector system.
Referring now to FIG. 4, shown therein is a schematic of a basic transducer layout 70 contained within dewar 71 in accordance with a principal teaching of the invention. As suggested in the foregoing paragraphs, an N×N infrared focal plane array 73 and N×N reflective spatial light modulator 75 may be disposed within dewar 71 and interconnected by amplifier bank 77 and buses 78,79. Array 73 and amplifier bank 77 may be carried on IC chip or ceramic carrier 80 as would occur to the skilled artisan practicing the invention. Counter 81 interconnects inputs 39-42 and multiplexers 83,84 connected by buses 86,87 to modulator 75 and array 73.
In the operation of the arrangement suggested in FIG. 4, at the application of power, counter 81 is initially reset to mark the beginning of a frame period and increases in value at the occurrence of each following cycle of the system clock. The value impressed upon counter 81 is decoded by multiplexers 83,84 which allows a single line for data from a row or column (depending on read-out structure) to be applied to a row of electrodes within array 73. The set of column or row data is then presented to amplifier bank 77 which amplifies the signals for transmission over bus 78 to modulator 75 and applied to the corresponding row or column of reflective elements on modulator 75. The value on counter 81 is then increased on the next cycle of the system clock to enable the set of row or column data for transfer to modulator 75. The foregoing process following initial reset of counter 81 is then repeated for the rest of the rows or columns during the frame period until modulator 75 contains the image transferred from array 73. Modulator 75 is then illuminated from outside dewar 71 by a low power laser (61 of FIG. 2). The laser light reflected by modulator 75 (beam 61' of FIG. 2) is encoded with an image from array 73 and is directed a detector system as suggested above. The process described within this paragraph defines one frame period, and counter 81 is again reset and the entire sequence is repeated for each following frame period. Since data from array 73 is transferred outside dewar 71 using no data lines, the number of operating leads (39-42) is but four.
FIG. 5 illustrates an alternative transducer system 90 within dewar 91 using two dimensional infrared focal plane array 93 and one dimensional modulator 95 for two dimensional to one dimensional data transfer according to an aspect of the invention. In operation of system 90, at the application of power, counter 101 is initially reset to mark the beginning of a frame period and increases in value at the occurrence of each following cycle of the system clock. The value impressed on counter 101 is decoded by multiplexer 104 which enables a single line for data from a row or column (depending on read-out structure) to be applied to a row of electrodes within array 93. The set of column or row data is then presented to amplifier bank 97 which amplifies the signals for transmission over bus 98 to linear modulator 95. Modulator 95 is then illuminated by a low power laser (61 of FIG 2), the reflected beam (beam 61' of FIG. 2) being encoded with an image of a single row of array 93 and directed a detector system. The value on counter 101 is then increased on the next cycle of the system clock to enable the next row or column for transfer to modulator 95. The process is then repeated for the remaining rows during the frame period until the entire image from array 93 is transferred to the digital or optical processor external of dewar 91. Counter 101 is then reset to the first row of array 93 and the sequence repeated for each following frame period.
FIG. 6 illustrates yet another transducer system 110 within dewar 111 using one dimensional infrared focal plane array 113 and two dimensional modulator 115 for one dimensional to two dimensional data transfer according to yet another aspect of the invention. No counter is needed for array 113 since but a single line of information exists therein. The clock cycle may be used to cycle array 113. Counter 121 records the image gathered by array 113 on modulator 115. In the operation of system 110, the clock signal activates transfer of data to the row electrodes of array 113 and counter 121 of modulator 115 is set to a value corresponding to the first row of the image to be scanned. The row data from array 113 is then transferred to the amplifier bank 117 for transmission to modulator 115 and applied to the row of modulator 115 corresponding to the row in the image being scanned. The value on counter 121 is then increased to coincide with the next row of imagery from (linear) array 113, and the foregoing process is repeated until modulator 115 contains the entire image scanned by array 113. Modulator 115 is then illuminated by a low power laser as above to encode the reflected beam with the image stored in modulator 115 and to direct the encoded beam to a detector, which marks the end of a frame period. Counter 121 is then reset to the top row of modulator 115 and the sequence repeated for each following frame period.
FIG. 7 illustrates another transducer system 130 within dewar 131 using one dimensional infrared focal plane array 133 and one dimensional modulator 135 for one dimensional to one dimensional data transfer according to the invention. No counter is needed in system 130 since there is only a single line of information. The clock cycle is used to cycle array 133 and modulator 135. In operation of system 130, the clock signal activates data transfer to the row electrodes of array 133. The row data is amplified by amplifier bank 137 and transmitted to modulator 135. Modulator 135 is then illuminated by a low power laser as above to encode the reflected beam with the image stored in modulator 135 and to direct the encoded beam to a detector.
The invention therefore provides an improved cryogenic dewar and optical data transducer system configured with a minimum number of electrical input leads and wherein data is efficiently extracted from the dewar optically and in parallel allowing high frame rates without corruption of the data during transmission. It is understood that modifications to the invention may be made as might occur to one with skill in the field of the invention within the scope of the appended claims. All embodiments contemplated hereunder which achieve the objects of the invention have therefore not been shown in complete detail. Other embodiments may be developed without departing from the spirit of the invention or from the scope of the appended claims.

Claims (8)

I claim:
1. A cryogenic data transducer system, comprising:
(a) a cryogenic dewar having optical window means therein for admitting an optical signal and a probe beam;
(b) an infrared focal plane array disposed within said dewar near said optical window means for receiving an optical signal from external of said dewar;
(c) a spatial light modulator disposed within said dewar near said optical window means, said spatial light modulator being operatively connected to said infrared focal plane array;
(d) a source of a collimated laser beam source and optical means for directing a probe beam from said source onto said spatial light modulator through said optical window means and directing a reflected beam external of said dewar from said spatial light modulator; and
(e) detection means for detecting and analyzing said reflected beam.
2. The system of claim 1 further comprising a cryogen within said dewar for maintaining the temperature of said infrared focal plane array below about -200°C.
3. The system of claim 2 wherein said cryogen is selected from the group consisting of liquid argon, liquid nitrogen and liquid helium.
4. The system of claim 1 wherein said spatial light modulator comprises a deformable mirror array operatively connected to said infrared focal plane array and responsive thereto.
5. In a cryogenic data transducer system including a cryogenic dewar and an infrared sensor array disposed within the dewar for receiving an optical signal external of the dewar, an improvement comprising:
(a) optical window means on said dewar for admitting a probe beam;
(b) a spatial light modulator disposed within said dewar near said optical window means, said spatial light modulator being operatively connected to and responsive to said infrared sensor array;
(c) a source of a collimated laser beam source and optical means for directing a probe beam from said source onto said spatial light modulator through said optical window means and directing a reflected beam external of said dewar from said spatial light modulator; and
(d) detection means for detecting and analyzing said reflected beam.
6. The improvement of claim 5 further comprising a cryogen within said dewar for maintaining the temperature of said infrared focal plane array below about -200° C.
7. The improvement of claim 6 wherein said cryogen is selected from the group consisting of liquid argon, liquid nitrogen and liquid helium.
8. The improvement of claim 5 wherein said spatial light modulator comprises a deformable mirror array operatively connected to said infrared focal plane array and responsive thereto.
US07/772,199 1991-10-07 1991-10-07 Optical data transducer Abandoned USH1354H (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US07/772,199 USH1354H (en) 1991-10-07 1991-10-07 Optical data transducer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/772,199 USH1354H (en) 1991-10-07 1991-10-07 Optical data transducer

Publications (1)

Publication Number Publication Date
USH1354H true USH1354H (en) 1994-09-06

Family

ID=25094273

Family Applications (1)

Application Number Title Priority Date Filing Date
US07/772,199 Abandoned USH1354H (en) 1991-10-07 1991-10-07 Optical data transducer

Country Status (1)

Country Link
US (1) USH1354H (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5440139A (en) * 1994-03-02 1995-08-08 Grumman Aerospace Corporation Circuit for optically coupling a cryobenic detector array with processing circuitry and for increasing the dynamic range of detection
US6034370A (en) * 1996-07-02 2000-03-07 Messerschmidt; Robert G. Multisource infrared spectrometer
US10091440B1 (en) * 2014-05-05 2018-10-02 Lockheed Martin Corporation System and method for providing compressive infrared imaging
US11333557B2 (en) * 2020-04-23 2022-05-17 Raytheon Company Optically powered cryogenic focal plane array (FPA) with an optical data link

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5440139A (en) * 1994-03-02 1995-08-08 Grumman Aerospace Corporation Circuit for optically coupling a cryobenic detector array with processing circuitry and for increasing the dynamic range of detection
WO1995023992A1 (en) * 1994-03-02 1995-09-08 Grumman Aerospace Corporation Optically coupled detector imaging system
US6034370A (en) * 1996-07-02 2000-03-07 Messerschmidt; Robert G. Multisource infrared spectrometer
US10091440B1 (en) * 2014-05-05 2018-10-02 Lockheed Martin Corporation System and method for providing compressive infrared imaging
US11333557B2 (en) * 2020-04-23 2022-05-17 Raytheon Company Optically powered cryogenic focal plane array (FPA) with an optical data link

Similar Documents

Publication Publication Date Title
US6268883B1 (en) High speed infrared imaging system and method
US3806729A (en) Charge coupled device ir imager
US4939369A (en) Imaging and tracking sensor designed with a sandwich structure
US4996427A (en) Imager for simultaneously obtaining two images of differing color bands using a single photodetector area array
JPH07128696A (en) Programmable focal plane signal processor and system
USH1354H (en) Optical data transducer
US4596930A (en) Arrangement for multispectal imaging of objects, preferably targets
US6078356A (en) Frequency multiplexed data from detector array
US5589876A (en) Infrared imaging device readily removing optical system contributory component
JPH03246428A (en) Infrared video device
KR100864101B1 (en) Improved microblolmeter operating systne
US4712888A (en) Spatial light modulator systems
US6534758B2 (en) Electromagnetic wave detector using quantum wells and subtractive detectors
US4160907A (en) Thermo-optical far infrared system
JPS61186826A (en) Thermal imaging device
Mandl Advances in on-focal-plane A/D with low-power optical readout
Arens et al. A 10-μm infrared camera
Turner et al. CMOS photodetectors for correlation peak location
Mandl et al. LWIR focal plane with digital readout demonstrating a passive free-space optical readout link
Küveler et al. A matrix photodiode array to measure Doppler shifts of solar spectral lines
RU2152138C1 (en) Matrix thermal imaging unit
Rhodes et al. A new system for observing solar oscillations at the Mount Wilson Observatory: I. System design and installation
Deters et al. Charge transfer device star tracker applications
DETERS et al. Charge injection device star tracker applications
Chinnappan et al. Intensified CCD Camera Based Remote Guiding Unit for VBT and Observation of Speckles with ICCD

Legal Events

Date Code Title Description
STCF Information on status: patent grant

Free format text: PATENTED CASE