• 전자공학회논문지SC
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• 제37권3호
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• pp.63-71
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• 2000

모든 물체에서 방출되는 적외선을 감지하여 영상신호로 만들어 주는 적외선 감지 칩은 보편적으로 적외선감지 소자와 신호 취득 회로가 각기 다른 칩으로 제작되어 하이브리드 본딩 기법을 통해 만들어 진다. 본 논문에서는 신호 취득 회로의 설계 과정과 시뮬레이션 결과를 보여 주며, 실제 제작 결과, 6V의 인가 전압에서 설계 사양에 만족하는 동작 특성을 보임을 확인하였다. 제작된 신호 취득 회로를 이용하여 적외선 감지칩을 제작하고 이를 자체 제작한 열영상 시스템에 장착하여 열영상을 구현해 보았다. 얻어진 열영상은 고온과 상온의 물체에 대해서 인식이 가능한 수준이었으며, 열영상 시스템의 잡음 특성을 좀 더 개선할 경우 더나은 열영상을 얻을 수 있으리라 기대한다.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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• pp.825-827
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• 2003

Multi-Spectral Camera(MSC) is a payload on the KOMPSAT-2 satellite to perform the earth remote sensing. The instrument images the earth using a push-broom motion with a swath width of 15 km and a ground sample distance (GSD) of 1 m over the entire field of view (FOV) at altitude 685 Km. The instrument is designed to have an on-orbit operation duty cycle of 20% over the mission lifetime of 3 years with the functions of programmable gain/ offset and on-board image data compression/storage. The MSC instrument has one(1) channel for panchromatic imaging and four(4) channel for multi-spectral imaging covering the spectral range from 450nm to 900nm using TDI CCD Focal Plane Array (FPA). In this paper, the architecture and function of MSC hardware including electrical interface and the operation concept which have been established based on the mission requirements are described. And the design and the preparation of MSC system operation are analyzed and discussed.

• Geomechanics and Engineering
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• 제24권3호
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• pp.237-251
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• 2021

The main purpose of this study is to investigate the performance of the proposed hybrid teaching-learning based optimization algorithm on the optimum design of reinforced concrete (RC) cantilever retaining walls. For this purpose, three different design examples are optimized with 100 independent runs considering continuous and discrete variables. In order to determine the algorithm performance, the optimization results were compared with the outcomes of the nine powerful meta-heuristic algorithms applied to this problem, previously: the big bang-big crunch (BB-BC), the biogeography based optimization (BBO), the flower pollination (FPA), the grey wolf optimization (GWO), the harmony search (HS), the particle swarm optimization (PSO), the teaching-learning based optimization (TLBO), the jaya (JA), and Rao-3 algorithms. Moreover, Rao-1 and Rao-2 algorithms are applied to this design problem for the first time. The objective function is defined as minimizing the total material and labor costs including concrete, steel, and formwork per unit length of the cantilever retaining walls subjected to the requirements of the American Concrete Institute (ACI 318-05). Furthermore, the effects of peak ground acceleration value on minimum total cost is investigated using various stem height, surcharge loads, and backfill slope angle. Finally, the most robust results were obtained by HTLBO with 50 populations. Consequently the optimization results show that, depending on the increase in PGA value, the optimum cost of RC cantilever retaining walls increases smoothly with the stem height but increases rapidly with the surcharge loads and backfill slope angle.

• 한국컴퓨터정보학회논문지
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• 제20권3호
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• pp.97-106
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• 2015

본 논문에서는 DIRCM의 개발단계에서 수행하는 기만 성능검증을 위한 시뮬레이터인 위협체모사기 구축에 관한 내용에 대해 기술한다. 기존의 PC기반의 성능분석 시뮬레이터와 달리 본 연구에서 개발된 위협체모사기는 DIRCM의 레이저를 실제 운용하는 거리에서 직접 조사하는 방식으로 실제 환경에서 기만효과를 정확히 분석 할 수 있다. 또한, 실험실에서 시준기를 통해 레이저를 조사하는 방식의 기만효과 시험도 가능하도록 개발하여 기만코드 개발에 필요한 시간과 비용을 절약할 수 있도록 하였다. 본 연구에서 개발한 위협체모사기는 실제 1,2세대 탐색기와 같은 F넘버와 같은 구조의 반사광학계로 개발하였다. 그리고 코드재밍 기법에 대한 성능분석 기능과 4세대 이상의 탐색기에 적용되는 면형검출기의 포화기만 분석도 가능한 구조로 개발하였다. 실험결과, 1,2세대 모의위협체는 정확한 추적성능과 기만효과를 나타내었다.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 1999년도 Proceedings of International Symposium on Remote Sensing
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• pp.375-380
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• 1999

Ocean Scanning Multispectral Imager (OSMI) is a payload on the KOMPSAT satellite to perform worldwide ocean color monitoring for the study of biological oceanography. The instrument images the ocean surface using a wisk-broom motion with a swath width of 800 km and a ground sample distance (GSD) of<1km over the entire field of view (FOV). The instrument is designed to have an on-orbit operation duty cycle of 20% over the mission lifetime of 3 years with the functions of programmable gain/offset and on-board image data compression/storage. The instrument also performs sun and dark calibration for on-board instrument calibration. The OSMI instrument is a multi-spectral imager covering the spectral range from 400nm to 900nm using CCD Focal Plane Array (FPA). The ocean colors are monitored using 6 spectral channels that can be selected via ground commands. KOMPSAT satellite with OSMI was integrated and the satellite level environment tests and instrument aliveness/functional test as well, such as launch environment, on-orbit environment (Thermal/vacuum) and EMl/EMC test were performed at KARI. Test results met the requirements and the OSMI data were collected and analyzed during each test phase. The instrument is launched on the KOMPSAT satellite in the late 1999 and the image is scheduled to start collecting ocean color data in the early 2000 upon completion of on-orbit instrument checkout.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2011년도 한국우주과학회보 제20권1호
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• pp.23.4-23.4
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• 2011

MIRIS is the main payload of the Science and Technology Satellite-3 (STSAT-3). which is being developed by KASI for infrared survey observation of the Galactic plane at Paschen alpha wavelength. Wideband filters in I and H band will also be used to observe cosmic infrared background. The MIRIS will perform astronomical observations in the near-infrared wavelengths of 0.9~2 ${\mu}m$ using a 256 ${\times}$ 256 Teledyne PICNIC FPA sensor providing a 3.67 ${\times}$ 3.67 degree field of view with a pixel scale of 51.6 arcsec. The flight model of the MIRIS has been recently developed, The system performance tests have been made in the laboratory, including opto-mechanics test, vibration test, thermal vacuum test and passive cooling test down to 200K, using a thermally controlled vacuum chamber. Several focus tests showed good agreements compared to initial design parameters. Recent efforts are being concentrated to improve the system performances, particularly to reduce readout noise level in electronics. After assembly and integration into the satellite bus, the MIRIS will be launched in 2012.

• 센서학회지
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• 제27권5호
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• pp.311-316
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• 2018

An antenna-coupled bolometer-type terahertz sensor was designed, fabricated, evaluated, and utilized to obtain terahertz transmission images. The sensor consists of a thin film bowtie antenna that resonates accordingly in response to an incident terahertz beam, a heater that converts the applied current in the antenna into heat, and a microbolometer that converts the rise in temperature into a change in resistance. The device is fabricated by a bulk micromachining process on a 4-inch silicon wafer. The fabricated sensor chip has a size of $2{\times}2mm$ and an active area of $0.1{\times}0.1mm^2$. The temperature coefficient of resistance (TCR) of the bolometer film (VOx) is 2.0%, which is acceptable for bolometer applications. The output sensor signal is proportional to the power of the incident terahertz beam. Transmission images were obtained with a 2-axis scanning imaging system that contained the sensor. The small active area of the sensor will enable the development of highly sensitive focal plane array sensors in terahertz imaging cameras in the future.

• Journal of Astronomy and Space Sciences
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• 제31권2호
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• pp.177-186
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• 2014

The Immersion Grating Infrared Spectrometer (IGRINS) is a near-infrared wide-band high-resolution spectrograph jointly developed by the Korea Astronomy and Space Science Institute and the University of Texas at Austin. IGRINS employs three HAWAII-2RG Focal Plane Array (H2RG FPA) detectors. We present the design and fabrication of the detector mount for the H2RG detector. The detector mount consists of a detector housing, an ASIC housing, a Field Flattener Lens (FFL) mount, and a support base frame. The detector and the ASIC housing should be kept at 65 K and the support base frame at 130 K. Therefore they are thermally isolated by the support made of GFRP material. The detector mount is designed so that it has features of fine adjusting the position of the detector surface in the optical axis and of fine adjusting yaw and pitch angles in order to utilize as an optical system alignment compensator. We optimized the structural stability and thermal characteristics of the mount design using computer-aided 3D modeling and finite element analysis. Based on the structural and thermal analysis, the designed detector mount meets an optical stability tolerance and system thermal requirements. Actual detector mount fabricated based on the design has been installed into the IGRINS cryostat and successfully passed a vacuum test and a cold test.

• JSTS:Journal of Semiconductor Technology and Science
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• 제13권4호
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• pp.303-317
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• 2013

Two novel clocking strategies for a high-speed multi-channel serializer-deserializer (SERDES) are proposed in this paper. Both of the clocking strategies are based on groups, which facilitate flexibility and expansibility of the SERDES. One clocking strategy is applicable to moderate parallel I/O cases, such as high density, short distance, consistent media, high temperature variation, which is used for the serializer array. Each group within the strategy consists of a full-rate phase-locked loop (PLL), a full-rate delay-locked loop (DLL), and two fixed phase alignment (FPA) techniques. The other is applicable to more awful I/O cases such as higher speed, longer distance, inconsistent media, serious crosstalk, which is used for the deserializer array. Each group within the strategy is composed of a PLL and two DLLs. Moreover, a half-rate version is chosen to realize the desired function of 1:2 deserializer. Based on the proposed clocking strategies, two representative ICs for each group of SERDES are designed and fabricated in a standard $0.18{\mu}m$ CMOS technology. Measurement results indicate that the two SERDES ICs can work properly accompanied with their corresponding clocking strategies.

• 항공우주기술
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• 제11권1호
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• pp.98-102
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• 2012

비냉각형 열상 시스템에 대한 관심이 국방 및 항공우주 분야에서 증가하고 있다. 특히, 국방분야 무기체계에서는 무인화 및 주야간 적군 탐지를 위한 요소기술로 활용되고 있다. 비냉각형 열상 시스템의 연구 분야 중 저비용, 저전력, 소형화를 위한 비냉각형 TEC(Thermal Electric Cooler)-less 열상 시스템에 대한 연구가 활발히 진행되고 있다. 그러나 TEC-less로 운영하기 위해서는 최적화된 불균일보정 계수의 추출 및 적용이 요구된다. 본 논문에서는 TEC-less로 최적화 된 보정 계수 획득 방법으로 선형 보간법을 이용한 보정 계수 추정 방법인 DCCE-LI(Dynamic Calibration Coefficient Estimation with Linear Interpolation)을 제안하고, 실험을 통해 제안 기법이 기존의 정적 보정 계수를 적용한 것에 비해 IR 영상 품질이 우수하고, 실시간 보정 계수 추정이 가능함을 보인다.