• Proceedings of the KSRS Conference
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• v.1
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• pp.228-231
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• 2006

In this paper, requirements of Meteorological Administration about Meteorological Imager (MI) of Communications, Ocean and Meteorological Satellite (COMS) is analyzed for the design of COMS ground station and according to the analysis results, the distribution image size of each observation area suitable for satellite Field Of View (FOV) stated at the requirements of meteorological administration is determined and the precise satellite FOV and the size of distribution image is calculated on the basis of the image size of the determined observation area. The results in this paper were applied to the detailed design for COMS ground station and also are expected to be used for the future observation scheduling and the scheduling of distribution of user data.

• Proceedings of the KSRS Conference
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• v.1
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• pp.257-259
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• 2006

The Communication Ocean Meteorological Satellite (COMS) is a geostationary satellite being developed by Korea Aerospace Research Institute. Geostationary Ocean Color Imager (GOCI) is one of the payloads embarked on the COMS satellite. It acquires ocean images around Korea in 8 visible spectral bands with a spatial resolution of about 500 m. The acquired data are used to provide forecasting and now casting of the ocean state. The GOCI operations are controlled by the satellite embedded software, i.e. on-board software. This paper introduces the GOCI payload of the COMS satellite and describes the control software for the GOCI.

• Proceedings of the KSRS Conference
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• v.1
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• pp.267-270
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• 2006

COMS has two imaging payloads, MI (Meteorological Imager) and GOCI (Geostationary Ocean Colour Imager). In GOCI case, data are packaged per each slot - one part of 16 two-dimensional arrays for imaging sensors - so its generation algorithm is simple. But MI case, data are made up with sequences of 480 bit blocks and are transmitted to its ground station sequentially. Moreover there is no time information in each 480 bit MI block, so a system in its ground system should be attaching time information at received MI blocks. DM (Decomposition Module) is one module of IMPS that receives Raw Data from DATS and generates Level 0 Products that include time tagging. This paper explains DM design for MI of COMS payloads.

• Proceedings of the KSRS Conference
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• 2008.10a
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• pp.100-103
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• 2008

COMS(Communication, Ocean and Meteorological Satellite) has multiple payloads; Meteorological Image(MI), Ocean Color Imager(GOCI) and Ka-band communication payloads. MI has 4 IR and 1 visible channel. In order to improve the quality of IR image, two calibration sources are used; black body image and cold space look data. In case of COMS, the space look is performed at 10.4 degree away from the nadir in east/west direction. During space look, SUN or moon intrusions are strictly forbidden, because it would degrade the quality of collected IR channel calibration data. Therefore we shall pay attention to select space look side depending on SUN and moon location. This paper proposes and discusses a simple and complete space look side selection logic based on SUN and moon intrusion event file. Computer simulation has been performed to analyze the performance of the proposed algorithm in term of east/west angular distance between space look position and hazardous intrusion sources; SUN and moon.

• Journal of Satellite, Information and Communications
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• v.3 no.2
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• pp.26-31
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• 2008

As a multi-mission GEO satellite, Communication, Ocean, and Meteorological Satellite (COMS) is scheduled to be launched in the year 2009. COMS has three different payloads: Ka-band communication payload, Geostationary Ocean Color Imager (GOCI) and Meteorological Imager (MI). Among the three payloads, MI and GOCI have several conflict relationships; one of them is that if MI mirror moves vertically larger than 4 Line Of Sight (LOS) angle while GOCI is imaging, image quality of GOCI becomes degraded. In this paper, MI scheduling algorithm to prevent GOCI's image quality degradation will be presented.

• Proceedings of the Optical Society of Korea Conference
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• 2008.02a
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• pp.71-72
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• 2008

과학기술위성3호 부탑재체로 영상분광기(COMIS, Compact Hyperspectral Imager)가 선정되어 2007년 5월부터 개발이 진행되고 있다. COMIS는 2010년 과학기술위성3호에 탑재 발사되어, 위성 궤도 700km 상공에서 해상도 30m을 가지고, 30km 폭의 지표면 또는 대기를 관측할 수 있다. 현재까지 국내에서 개발된 위성탑재 지구관측카메라가 흑백이거나 다분광(3파장)으로 지구관측을 하는 것에 반하여 COMIS는 가시광 및 근적외선 영역에서 16${\sim}$62대역(4${\sim}$15nm 파장 분해능)의 초분광 관측을 수행하게 된다. 초분광 영상은 관측 대상 물성의 상세 구분이 가능한 관계로 군사적 활용을 포함한 원격 탐사의 주요 활용 분야로 대두되고 있다. 본 논문은 과학기술위성3호 부탑재체로 개발되는 영상분광기인 COMIS(Compact Hyperspectral Imager)의 전반적인 개념, 활용 과학을 먼저 소개하고 상세 광학 설계를 발표한다.

• Korean Journal of Optics and Photonics
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• v.6 no.3
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• pp.173-177
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• 1995

The scanning type modulation transfer function (MTF) measurement system of linear charge coupled device (CCD) imagers is fabricated and the MTF of a linear CCD imager is tested. Measured MTF values are very sensitive to small angle knife-edge skew within 1 degree and show different results in several wavelengths. The MTF of the linear CCD imager is measured in different color temperatures of a tungsten filament lamp and the MTF uniformity of ti,t eel) pixels is tested.tested.

• Journal of the Korea Institute of Military Science and Technology
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• v.9 no.2 s.25
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• pp.111-117
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• 2006

This paper describes the design principles and methods of electronic processor for thermal imager with 320$\times$240 staring array infrared detector. For the detector's nonuniformity correction and excellent image quality, we have designed the multi-point correction method using the defocusing technique of the optics. And to enhance the image of low contrast and improve the detection capability, the new technique of histogram processing has been designed. Through these image processing techniques, we have developed the high quality thermal imager and acquired a satisfactory thermal image. The result of MRTD(Minimum Resolvable Temperature Difference) is $0.1^{\circ}C$ at 4cycles/mard.

• Proceedings of the Optical Society of Korea Conference
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• 2000.08a
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• pp.54-55
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• 2000

해양관측카메라 Ocean Scanning Multi-spectral Imager (OSMI)를 탑재한 다목적 실용위성(KOMPSAT) 1호기가 1999년 12월 21일 발사되었다. OSMI는 유연한 임무 수행을 위해 궤도운영중에 관측파장대역 선택과 응답 이득 조정이 가능하도록 설계되었다. 또한 OSMI는 기기 노화 등에 따른 성능 변화 감지 및 보정을 위해 태양광 보정을 궤도운영중 수행한다. 여러 이득 단계에 대해 발사후 복사 응답 특성을 기기 보정 측면에서 연구하였다. 발사전 실험실 성능 측정 결과에 근거하여 발사후 초기 운영 단계에서 측정한 태양광 보정 자료의 선형 curve fitting을 통해 발사후 복사 응답 특성을 분석하였다. 이 분석은 OSMI 기기 보정 및 영상 품질 이해에 유용할 것이다.

• Nuclear Engineering and Technology
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• v.55 no.2
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• pp.648-654
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• 2023

A dual-particle imager (DPI) is configured in a hand-held form factor, then one can efficiently and conveniently deploy the DPI to detect the presence of special nuclear materials (SNM) and identify any isotopic variations that differ from their natural abundances. Here we show that by maximizing the areal coupling between a pixelated scintillator array and the partitioned photosensor readout such as a silicon photomultiplier (SiPM), the information utilization of the gamma-ray and neutron information in the radiation field can be enhanced, thus enabling one to rapidly acquire spatial maps of the distributions on gamma-ray and neutron emitters.