• 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.

• 대한원격탐사학회지
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• 제18권1호
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• pp.53-59
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• 2002

The 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 GSD(Ground Sample Distance) of 1 m over the entire FOV(Field Of View) at altitude 685 km. The instrument is designed to haute 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 channel for panchromatic imaging and four channel for multi-spectral imaging covering the spectral range from 450nm to 900nm using TDI(Time Belayed Integration) CCD(Charge Coupled Device) FPA(Focal Plane Assembly). The MSC hardware consists of three subsystem, EOS(Electro Optic camera Subsystem), PMU(Payload Management Unit) and PDTS(Payload Data Transmission Subsystem) and each subsystems are currently under development and will be integrated and verified through functional and space environment tests. Final verified MSC will be delivered to spacecraft bus for AIT(Assembly, Integration and Test) and then COMSAT-2 satellite will be launched after verification process through IST(Integrated Satellite Test). In this paper, the introduction of MSC, the configuration of MSC electronics including electrical interlace and design of CEU(Camera Electronic Unit) in EOS are described. MSC Operation parameters induced from the operation concept are discussed and analyzed to find the influence of system for on-orbit operation in future.

• 대한원격탐사학회지
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• 제15권4호
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• pp.297-305
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• 1999

Ocean Scanning Multispectral Imager (OSMI) is a payload on the KOMPSAT satellite to perform global 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 800km 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 including instrument aliveness/functional test, such as launch environment, on-orbit environment (Thermal/Vacuum) and EMI/EMC test were performed at KARl. 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 on December 21,1999 and is scheduled to start collecting ocean color data in the early 2000 upon completion of on-orbit instrument checkout.

• 한국인터넷방송통신학회논문지
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• 제22권6호
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• pp.107-112
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• 2022

드론과 같은 임베디드 시스템에서 데이터를 서버로 전송해 실시간 분석을 진행함에 있어진행하는 데 초분광 영상 전체를 저장, 전송, 분석하는 데 전력 소모와 시간이 많이 소요되어 어려움이 있다. 그래서 초분광 영상 데이터는 차원 축소 또는 압축 전처리를 통해 서버로 전송하게 된다. 분석에 필요한 밴드만 보내기 위해서는 피처 선택 기법을 사용하는데 이러한 알고리즘은 대게 효율은 높더라도 영상 크기에 따라 처리 시간이 매우 소요가 크다. 본 논문에서는 밴드선택 알고리즘의 시간적인 단점을 개선하여한 기댓값 기반의 알고리즘을 제안한다. 실험 결과 8GB 데이터의 40000*682 해상도 이미지 기준 평균 소요 시간인 24시간을 60~180초 내외로 감소시키고, 150개 밴드 중에 45개를 활용하여 7.6GB 램 사용을 2.3GB로 크게 감소시켰다. 시간은 크게 줄였음에도 픽셀 분류 성능은 기존과 유사하게 98% 이상의 분석 결과를 도출하였다.

• 한국통신학회논문지
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• 제33권9C호
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• pp.691-696
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• 2008

본 논문은 AMR(Adaptive Multi Rate)코더의 7.4kit/s 모드를 기반으로 화자 의존적인 환경에서 더욱 압축률을 높인 새로운 켈프(CELP)계열의 코더를 제안한다. 제안된 코더는 OGM(OutGoing Message)이나 TTS(Text-To-Speech) 등 한 사람의 음성만을 필요로 하는 시스템에서 유용하게 사용할 수 있다. 새로운 코더의 압축률을 높이기 위해서 무감독 학습 신경망인 Centroid Neural Networks(CNN)를 이용한 새로운 LSP 코드북을 생성하여 사용한다. 또한 고정 코드북 탐색 단계에서 AMR 7.4 kbit/s 모드에서는 4개의 펄스를 서브프레임 마다 사용하는 대신에 새로운 코더에서는 오직 2개의 펄스만을 사용하기 때문에 압축률을 더 높일 수 있다. 이로 인해서 스피치의 질이 감소하게 되는데, 각 서브프레임 마다 예상하는 펄스를 적용함으로써 보상받을 수 있다. 제안된 보코더는 기존 AMR 7.4Kbps모드와 비교해 27% 높은 압축률을 가지는 동시에, MOS( Mean Opinion Score)의 면에서 볼 때, 대등한 음질을 보였다.

• 천문학회지
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• 제37권5호
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• pp.471-476
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• 2004

We propose an analytical model to estimate the influence of a merger on the thermal SZ effect. Following observations we distinguish between subsonic and transonic mergers. Using analytical velocity fields and the Bernoulli equation we calculate the excess pressure around a moving subcluster for an incompressible subsonic gas. Positive excess around the stagnation point and negative excess on the side of the subcluster lead to characteristic signatures in the SZ map, of the order of $10\%$ compared to the unperturbed signal. For a transonic merger we calculate the change in the thermal spectral SZ function, resulting from bow shock accelerated electrons. The merger shock compression factor determines the power law tail of the new non-thermal electron population and is directly related to a shift in the crossover frequency. This shift is typically a few percent towards higher frequencies.

• 한국광학회지
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• 제10권1호
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• pp.58-63
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• 1999

광반도체 증폭기를 이용하여 $1.5\mu\textrm{m}$파장 영역에서 발전하는 조화 모드 록킹된 10GHz 고리형 반도체-광섬유 레이저를 구현하였다. 레이저 펄스폭은 13~18ps이고, 파장 선폭은 0.4~0.6nm이며, 양으로 주파수 처핑되었다. 2km 길이의 표준단일 모드 광섬우를 이용하여 4dBm의 평균 출력을 갖는 레이저 펄스를 광섬유의 군분산 보상에 의해 펄스폭을 최대 6.8ps까지 압축시켰다.

• 한국통신학회논문지
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• 제34권7C호
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• pp.649-653
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• 2009

디지털 영상은 영상압축이나 기타 다양한 디지털 처리에 용이한 장점이 있는 반면 위/변조가 상대적으로 용이하기 때문에 그에 대한 대응을 위한 다양한 디지털 워터마킹 기법이 개발되었다. 워터마킹 기법은 공간 또는 주파수 영역에서의 다양한 적용에 가능한데, 본 연구에서는 디지털 콘텐츠 대부분이 압축되어 전송, 저장되는 추세와, 최근 대부분의 멀티미디어 동영상 코덱 표준으로 채택이 되고 있는 H.264/AVC 언코더를 기반으로 한 워터마크 삽입을 실시간으로 수행하기 위한 기법을 제시한다.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2004년도 Proceedings of ISRS 2004
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• pp.457-459
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• 2004

The Channel Coding Unit (CCU) is an integral component of Payload Data Transmission System (PDTS) for the Multi-Spectral Camera (MSC) data. The main function of the CCU is channel coding and encryption. CCU has two channels (I & Q) for data processing. The input of CCU is the output of DCSU (Data Compression & Storage Unit). The output of CCU is the input of QTX which modulate data for RF communication. In this paper, there are the overview, short H/W description and operation concept of CCU.

• 천문학회지
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• 제48권1호
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• pp.9-20
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• 2015

We study the evolution of the energy spectrum of cosmic-ray electrons accelerated at spherically expanding shocks with low Mach numbers and the ensuing spectral signatures imprinted in radio synchrotron emission. Time-dependent simulations of diffusive shock acceleration (DSA) of electrons in the test-particle limit have been performed for spherical shocks with parameters relevant for typical shocks in the intracluster medium. The electron and radiation spectra at the shock location can be described properly by the test-particle DSA predictions with instantaneous shock parameters. However, the volume integrated spectra of both electrons and radiation deviate significantly from the test-particle power-laws, because the shock compression ratio and the flux of injected electrons at the shock gradually decrease as the shock slows down in time. So one needs to be cautious about interpreting observed radio spectra of evolving shocks based on simple DSA models in the test-particle regime.