• 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.

• 정보처리학회논문지:소프트웨어 및 데이터공학
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• 제10권10호
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• pp.429-438
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• 2021

최근 실감 콘텐츠는 디스플레이 기술의 발달에 따라 다양한 방식으로 적용되고 있으며 높아지는 대중의 요구에 따라 최종적 실감 콘텐츠 기술인 홀로그램이 제한적으로 사용되고 있다. 그러나 대부분의 실감 콘텐츠에는 HMD(head mounted device) 또는 안경 형태의 디바이스가 요구되며 기타의 실감 콘텐츠 디스플레이 기술은 체험 공간에서의 단일 이미지 평면을 사용자에게 전달하므로 단조로운 콘텐츠 체험을 제공한다. 이에 본 논문에서는 다양한 실감 콘텐츠 기술과 홀로그램 기술이 적용된 실감 콘텐츠를 정리하고, 프로젝션 맵핑과 플로팅 홀로그램을 융합한 상호작용 기반의 체험형 실감 콘텐츠 서비스를 제안한다. 프로젝션 맵핑되는 스크린과 다중 플로팅 홀로그램 생성 장치를 통해 사용자 시점에서의 깊이 방향이 확장된 3차원 입체 공간을 제공함과 동시에 사용자의 신체 전체와 부분적 모션을 다수의 센서를 통해 인식가능하게 하여 기존 대비 사용자의 활동 영역이 확장된 상호작용 콘텐츠 서비스가 실현이 가능하도록 설계하였다.

• 방송공학회논문지
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• 제24권4호
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• pp.580-591
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• 2019

본 논문의 목적은 자율주행을 위하여 카메라와 라이다를 이용하여 객체를 검출하고 각 센서에서 검출된 객체를 late fusion 방식으로 융합을 하여 성능을 향상하는 것을 목적으로 한다. 카메라를 이용한 객체 검출은 one-stage 검출인 YOLOv3을, 검출된 객체의 거리 추정은 perspective matrix를, 라이다의 객체 검출은 K-means 군집화 기반 객체 검출을 각각 이용하였다. 카메라와 라이다 calibration은 PnP-RANSAC을 이용하여 회전, 변환 행렬을 구하였다. 센서 융합은 라이다에서 검출된 객체를 이미지 평면에 옮겨 Intersection over union(IoU)을 계산하고, 카메라에서 검출된 객체를 월드 좌표에 옮겨 거리, 각도를 계산하여 IoU, 거리 그리고 각도 세 가지 속성을 로지스틱 회귀를 이용하여 융합을 하였다. 융합을 통하여 각 센서에서 검출되지 않은 객체를 보완해주어 성능이 약 5% 증가하였다.

• International Journal of Internet, Broadcasting and Communication
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• 제13권1호
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• pp.47-53
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• 2021

Gait kinematics and kinetics have a similar tendency between men and women, yet it remains unclear how walking while carrying a load affects the gait mechanism. Twenty adults walked with preferred velocity on level ground of 20 m relative to change of a load carriage (no load, 15%, 30% of the body weights) aimed to observe gait mechanism. We measured gait posture using the three-dimensional image analysis and ground reaction force system during stance phase on left foot. In main effect of gender difference, men showed increased displacement of center of gravity (COG) compared to women, and it showed more extended joint angle of hip and knee in sagittal plane. In main effect of a load difference, knee joint showed more flexed postuel relative to increase of load carriage. In main effect of load difference on the kinetic variables, medial-lateral force, anterior-posterior force (1st breaking, 2nd propulsive), vertical force, center of pressure (COP) area, leg stiffness, and whole body stiffness showed more increased values relative to increase of load carriage. Also, men showed more increased COP area compared to women. Interaction showed in the 1st anterior-posterior force, and as a result of one-way variance analysis, it was found that a load main effect had a greater influence on the increase in the magnitude of the braking force than the gender. The data in this study explains that women require little kinematic alteration compared to men, while men in more stiff posture accommodate an added load compared to women during gait. Additionally, it suggests that dynamic stability is maintained by adopting different gait strategies relative to gender and load difference.

• 정보보호학회논문지
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• 제21권6호
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• pp.171-181
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• 2011

본 논문에서는 감시영역을 벗어난 후 다시 돌아온 객체에 대한 배회행위를 효과적으로 인식 할 수 있는 지능형 배회행위 검출 시스템을 제안한다. 전경과 배경을 가우시안 혼합 모델을 이용하여 분리하고 그림자를 제거하여 객체를 인식한 후, 객체의 색도 히스토그램을 이용하여 감시영역을 벗어난 후 돌아온 객체들을 판단하고 감시영역에 존재하는 시간을 보전한다. 배회행위를 판단하기 위해 카메라 캘리브레이션을 통해 실세계 배회패턴과 같은 행태의 매크로 블록을 영상좌표에 도입한 후 배회궤적을 추출하고, 감시영역에 객체가 존재하는 시간을 함께 고려하여 배회행위를 판단한다. 제안하는 방법은 실험에 사용된 모든 배회행위 프레임에서 정확하게 배회행위를 검출하여 그 효과를 입증하였다.

• 한국지진공학회논문집
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• 제26권1호
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• pp.13-22
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• 2022

This study proposes a low-cycle fatigue life derived from measurement points on pipe elbows, which are components that are vulnerable to seismic load in the interface piping systems of nuclear power plants that use seismic isolation systems. In order to quantitatively define limit states regarding leakage, i.e., actual failure caused by low-cycle fatigue, in-plane cyclic loading tests were performed using a sine wave of constant amplitude. The test specimens consisted of SCH40 6-inch carbon steel pipe elbows and straight pipes, and an image processing method was used to measure the nonlinear behavior of the test specimens. The leakage lines caused by low-cycle fatigue and the low-cycle fatigue curves were compared and analyzed using the relationship between the relative deformation angles, which were measured based on each of the measurement points on the straight pipe, and the moment, which was measured at the center of the pipe elbow. Damage indices based on the combination of ductility and dissipation energy at each measurement point were used to quantitatively express the time at which leakage occurs due to through-wall cracking in the pipe elbow.

• 전기전자학회논문지
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• 제26권3호
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• pp.416-421
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• 2022

본 연구에서는 영상감시 장치에 액정 기반 편광 제어 기술을 결합하여 피사체에서 반사된 빛의 부분 선형 편광을 제거할 수 있는 편광 영상감치 장치 시스템을 제안한다. 빛의 편광 방향을 전기 광학적으로 변조하는 TN(Twisted Nematic) 액정을 사용하면 카메라 렌즈 앞에서 편광 필터를 기계적으로 회전할 필요가 없다. 이러한 기술을 사용하여 얻은 여러 편광 이미지는 컴퓨터 소프트웨어에 의해 이미지화된다. 또한 액정 패널은 사각형 형태로 생산되어 왔으나 대부분의 카메라 렌즈는 일반적으로 원형이고 렌즈 주변에 조명이나 기타 구동 장치가 설치되어 있어 원형 액정 패널을 적용하여 공간을 최적화하였다. 이 기술의 개발을 통해 전기적으로 전환 가능하고 공간에 최적화된 액정 편광 패널이 개발되었다.

• Current Optics and Photonics
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• 제6권2호
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• pp.171-182
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• 2022

A single-photon laser and mid-wave infrared (MWIR) common aperture optical system was designed and developed to detect and range a long-distance civil aviation aircraft. The secondary mirror of the Ritchey-Chretien (R-C) optical system was chosen as a dichroic lens to realize the design of a common aperture system for the laser and MWIR. Point spread function (PSF) ellipticity was introduced to evaluate the coupling efficiency of the laser receiving system. A small aperture stop and narrow filter were set in the secondary image plane and an afocal light path of the laser system, respectively, and the stray light suppression ability of the small aperture stop was verified by modeling and simulation. With high-precision manufacturing technology by single point diamond turning (SPDT) and a high-efficiency dichroic coating, the laser/MWIR common aperture optical system with a 𝜑300 mm aluminum alloy mirror obtained images of buildings at a distance of 5 km with great quality. A civil aviation aircraft detection experiment was conducted. The results show that the common aperture system could detect and track long-distance civil aviation aircraft effectively, and the coverage was more than 450 km (signal-to-noise ratio = 6.3). It satisfied the application requirements for earlier warning and ranging of long-range targets in the area of aviation, aerospace and ground detection systems.

• 천문학회보
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• 제46권1호
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• pp.57.3-58
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• 2021

We performed three-dimensional Monte Carlo dust scattering radiative transfer simulations for FUV light to obtain dust scattered FUV images and compared them with the observed FUV image obtained by FIMS/SPEAR and GALEX. From this, we find the scattering properties of interstellar dust in our Galaxy and suggest the intensity of extragalactic background light (EBL) at FUV wavelength. The best-fit values of the scattering properties of interstellar dust are albedo = 0.38^-0.04_+0.04, g-factor = 0.55^-0.15_+0.10, and EBL = 138^-23₊₂₁ CU for the allsky which are consistent well with the Milky Way dust model of Draine and direct measurements of Gardner et al., respectively. At the high Galactic latitude of |b|>10°, the observation is well fitted with the model of lower albedo = 0.35^-0.04_+0.06 and g-factor = 0.50^-0.20_+0.15. On the contrary, the scattering properties of interstellar dust show higher albedo = 0.43^-0.02_+0.02 and g-factor = 0.65^-0.15_+0.05 near the Galactic plane of |b|<10°. In the present simulation, recent three-dimensional distribution maps of interstellar dust in our Galaxy, stellar distances in the catalog of GAIA DR2, and FUV fluxes and/or spectral types in the TD-1 and Hipparcos star catalogs were used.