• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2008년도 International Symposium on Remote Sensing
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• pp.220-223
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• 2008

A camera system for the satellite application performs the mission of observation by measuring radiated light energy from the target on the earth. As a development stage of the system, the signal level analysis by estimating the number of electron collected in a pixel of an applied CCD is a basic tool for the performance analysis like SNR as well as the data path design of focal plane electronic. In this paper, two methods are presented for the calculation of the number of electrons for signal level analysis. One method is a quantitative assessment based on the CCD characteristics and design parameters of optical module of the system itself in which optical module works for concentrating the light energy onto the focal plane where CCD is located to convert light energy into electrical signal. The other method compares the design\ parameters of the system such as quantum efficiency, focal length and the aperture size of the optics in comparison with existing camera system in orbit. By this way, relative count of electrons to the existing camera system is estimated. The number of electrons, as signal level of the camera system, calculated by described methods is used to design input circuits of AD converter for interfacing the image signal coming from the CCD module in the focal plane electronics. This number is also used for the analysis of the signal level of the CCD output which is critical parameter to design data path between CCD and A/D converter. The FPE(Focal Plane Electronics) designer should decide whether the dividing-circuit is necessary or not between them from the analysis. If it is necessary, the optimized dividing factor of the level should be implemented. This paper describes the analysis of the electron count of a camera system for a satellite application and then of the signal level for the interface design between CCD and A/D converter using two methods. One is a quantitative assessment based on the design parameters of the camera system, the other method compares the design parameters in comparison with those of the existing camera system in orbit for relative counting of the electrons and the signal level estimation. Chapter 2 describes the radiometry of the camera system of a satellite application to show equations for electron counting, Chapter 3 describes a camera system briefly to explain the data flow of imagery information from CCD and Chapter 4 explains the two methods for the analysis of the number of electrons and the signal level. Then conclusion is made in chapter 5.

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2001년도 하계학술대회 논문집
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• pp.533-538
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• 2001

The ZnSe sample grown by chemical bath deposition (CBD) method were annealed in Ar gas at 450$^{\circ}C$ Using extrapolation method of X-ray diffraction pattern, it was found to have zinc blend structure whose lattice parameter a$\_$o/ was 5.6687 ${\AA}$. From Hall effect, the mobility was likely to be decreased by impurity scattering at temperature range from 10 K to 150 K and by lattice scattering at temperature range from 150 K to 29 3K. The band gap given by the transmission edge changed from 2.7005 eV at 293 K to 2.8739 eV at 10 K. Comparing photocurrent peak position with transmission edge, we could find that photocurrent peaks due to excition electrons from valence band, $\Gamma$$\_$8/ and $\Gamma$$\_$7/ to conduction band $\Gamma$$\_$6/ were observed at photocurrent spectrum. From the photocurrent spectra by illumination of polarized light on the ZnSe thin film, we have found that values of spin orbit coupling splitting Δso is 0.0981 eV. From the PL spectra at 10 K, the peaks corresponding to free bound excitons and D-A pair and a broad emission band due to SA is identified. The binding energy of the free excitons are determined to be 0.0612 eV and the dissipation energy of the donor -bound exciton and acceptor-bound exciton to be 0.0172 eV, 0.0310 eV, respectively.

• 한국임상수의학회지
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• 제20권2호
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• pp.145-149
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• 2003

개의 정상안혈관저항지수와 그 재현성을 측정하고자 컬러도플러 초음파를 이용하여 본 실험을 수행하였다. 내측 긴 후모양체 동맥, 모양체 동맥, 안동맥의 혈관저항지수의 정상범주를 측정하기 위하여 58두의 개에서 컬러도플러 초음파를 실시하였다. 정상견에서 내측 긴 후모양체동맥, 모양체동맥, 안동맥의 저항지수(%)를 측정한 결과, 그 수치는 각각 0.67$\pm$0.07, 0.70$\pm$0.06, 그리고 0.08$\pm$0.04이었으며, 모든 혈관의 저항지수는 좌우안구간에 차이가 없었으며, 성별이나 두개골 형태가 미치는 영향도 없는 것으로 판명되었다. 안혈관 저항지수의 반복측정에 따른 오차를 평가하기 위해서 4회 반복 측정한 결과, 안동맥저항지수의 반복측정변이계수가 4.1%로 가장 낮았으며 긴 후모양체동맥과 모양체동맥의 저항지수의 반복측정변이계수는 각각 12.9%와 7.8%로 모든 동맥에서 높은 재현성을 보였다. 이상의 결과로 보아, 컬러도플러 초음파가 개의 안구 및 안와의 혈순환에 대한 객관적인 측정자료를 제시하는데 매우 유용한 지표인 것으로 판단된다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2002년도 춘계학술대회논문집
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• pp.441-447
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• 2002

KSR-III(Korea Sounding Rocket - III), which is being developed by Space Technology R&D Division of KARI(Korea Aerospace Research Institute) will be launched in late 2002. It is a three-stage, liquid propellant rocket which can reach 250 km altitude and will carry out observation of ozone layer and scientific experiments, such as microgravity experiment, and atmospheric measurement. KSR-III is believed to be an intermediate to the launch vehicle capable of carrying a satellite to its orbit. Space Test Department of KARI performed GVT(Ground Vibration Test) fer KSR-III EM at Rocket Test Building of KARI. GVT is very important for predicting the behavior of rocket in its operation, developing flight control program and performing aerodynamic analysis. This paper gives an introduction of rocket GVT configuration and information on test procedures, techniques and results of It. In this test. to simulate free-free condition, test object hung in the air laterally by 4 bungee cords specially devised. For the excitation of test object, pure random signal by two electromagnetic shakers was used and total 22 frequency response functions were achieved. Polyreference parameter estimation was performed to identify the modal parameters with MIMO(Multi-Input-Multi-Output) method. As the result of the test, low frequency mode shapes and modal parameters below 60Hz were identified

• 대한화학회지
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• 제24권2호
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• pp.91-100
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• 1980

축방향대칭을 갖는 팔면체 $[Ti(III)A_3B_3]$형태 착물의 자기모멘트를 계산하는 식을 유도하여 distortion parameter$({\delta})$, 스핀-궤도 상호작용상수$({\zeta}')$ 및 orbital reduction factor의 실험치를 사용하여 이들 착물의 자기모멘트를 계산하였다. 축방향으로 일그러진 팔면체 $[Ti(III)A_3B_3]$형태 착물의 계산한 자기모멘트가 실험치와 비교적 일치하였다. 팔면체로부터 축방향 일그러짐이 커짐에 따라 그리고 orbital reduction factor가 감소함에 따라 계산한 자기모멘트의 값이 크게 감소하였다. 축방향대칭보다 낮은 리간드장으로 일그러진 팔면체착물의 자기모멘트를 계산하는 방법을 발전시켰으며 계산한 자기모멘트를 기초로 하여 일그러진 팔면체 $[Ti(III)A_3B_3]$형태 착물의 구조를 논의하였다.

• Bulletin of the Korean Chemical Society
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• 제18권12호
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• pp.1274-1280
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• 1997

The photodissociation dynamics of CH2I2 has been studied at 304 nm by state-selective photofragment translational spectroscopy. Velocity distributions, anisotropy parameters, and relative quantum yields are obtained for the ground I(2P3/2) and spin-orbit excited state I*(2P1/2) iodine atoms, which are produced from photodissociation of CH2I2 at this wavelength. These processes are found to occur via B1 ← A1 type electronic transitions. The quantum yield of I*(2P1/2) is determined to be 0.25, indicating that the formation of ground state iodine is clearly the favored dissociation channel in the 304 nm wavelength region. From the angular distribution of dissociation products, the anisotropy parameters are determined to be β(I)=0.4 for the I(2P3/2) and β(I*)=0.55 for the I*(2P1/2) which substantially differ from the limiting value of 1.13. The positive values of anisotropy parameter, however, show that the primary processes for I and I* formation channels proceed dominantly via a transition which is parallel to I-I axis. The above results are interpreted in terms of dual path formation of iodine atoms from two different excited states, i.e., a direct and an indirect dissociation via curve crossing between these states. The translational energy distributions of recoil fragments reveal that a large fraction of the available energy goes into the internal excitation of the CH2I photofragment; < Eint > /Eavl=0.80 and 0.82 for the I and I* formation channels, respectively. The quantitative analysis for the energy partitioning of available energy into the photofragments is used to compare the experimental results with the prediction of direct impulsive model for photodissociation dynamics.

• 천문학회보
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• 제44권1호
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• pp.65-65
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• 2019

Near-Earth objects consist of a mixture of bodies originated from outer solar system and main asteroidal belt, which are recognized as comets and near-Earth asteroids. In principal, they have orbits distinguishable by their orbital elements. It is, however, that some comets are recognized as asteroids because they could have lost the most of volatile materials in their subsurface layers. Due to their asteroidal appearances, it has been challenging to discriminate such dormant comets from a list of known asteroids. Here we propose to utilize polarimetric technique for finding such dormant comets. We thus conducted a polarimetric observations of three candidates of dormant comet nuclei, (331471) 1984 QY1, (3552) Don Quixote and (944) Hidalgo, by using the 1.6-m Pirka Telescope at the Nayoro observatory (operated by Hokkaido University, Japan). We selected these asteroids in comet-like orbits (ACOs) based on the orbital elements (i.e., the Tisserand parameter with respect to Jupiter TJ < 3). We found that 1984 QY1 has a polarimetric albedo (geometric albedo determined via polarimetry) pV = 0.16 +/- 0.06 while both Don Quixote and Hidalgo have Rc-band polarimetric albedos pR < 0.05. In accordance with the polarimetric result together with a dynamical analysis, we surmised that 1984 QY1 could be an S-type asteroid evolved into the current orbit via 3:1 mean motion resonance with Jupiter. On the contrary, the previous spectroscopic studies indicated that Don Quixote and Hidalgo are classified into D-type taxonomic group, which are typical of comet nuclei. In this presentation, we will introduce our polarimetric observations of ACOs and emphasize that polarimetry is powerful for discriminating the asteroidal and cometary origins.

• Journal of Positioning, Navigation, and Timing
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• 제13권2호
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• pp.189-197
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• 2024

Galileo is a European Global Navigation Satellite System (GNSS) that has offered the Galileo Open Service since 2016. Consequently, the standardization of GNSS augmentation systems, such as Satellite Based Augmentation System (SBAS), Ground Based Augmentation System (GBAS), and Aircraft Based Augmentation System (ABAS) for Galileo signals, is ongoing. In 2023, the European Union Space Programme Agency (EUSPA) released prior probabilities of a satellite fault and a constellation fault for Galileo, which are 3×10^-5 and 2×10^-4 per hour, respectively. In particular, the prior probability of a Galileo constellation fault is significantly higher than that for the GPS constellation fault, which is defined as 1×10^-8 per hour. This raised concerns about its potential impact on GBAS integrity monitoring. According to the Global Positioning System (GPS) Standard Positioning Service Performance Standard (SPS PS), a constellation fault is classified as a wide fault. A wide fault refers to a fault that affects more than two satellites due to a common cause. Such a fault can be caused by a failure in the Earth Orientation Parameter (EOP). The EOP is used when transforming the inertial axis, on which the orbit determination is based, to Earth Centered Earth Fixed (ECEF) axis, accounting for the irregularities in the rotation of the Earth. Therefore, a faulty EOP can introduce errors when computing a satellite position with respect to the ECEF axis. In GNSS, the ephemeris parameters are estimated based on the positions of satellites and are transmitted to navigation satellites. Subsequently, these ephemeris parameters are broadcasted via the navigation message to users. Therefore, a faulty EOP results in erroneous broadcast ephemeris data. In this paper, we assess the conventional ephemeris fault detection monitor currently employed in GBAS for wide faults, as current GBAS considers only single failure cases. In addition to the existing requirements defined in the standards on the Probability of Missed Detection (PMD), we derive a new PMD requirement tailored for a wide fault. The compliance of the current ephemeris monitor to the derived requirement is evaluated through a simulation. Our findings confirm that the conventional monitor meets the requirement even for wide fault scenarios.

• 센서학회지
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• 제10권1호
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• pp.62-70
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• 2001

CBD방법으로 성장하여 $450^{\circ}C$로 열처리한 ZnSe 박막은 회전 무늬로부터 외삽법으로 구한 격자상수 $a_0$가 $5.6678\;{\AA}$인 zinc blend임을 알았다. Van der Pauw 방법으로 측정한 Hall 데이터에 의한 이동도는 10 K에서 150 K 까지는 불순물 산란 (impurity scatterimg)에 의하여, 150 K에서 293 K까지는 격자산란 (lattice scattering)에 의하여 감소하는 경향을 나타냈다. 또한 운반자 농도의 ln n대 1/T에서 구한 활성화 에너지($E_a$)는 0.27 eV였다. 투과 곡선의 투과단으로 본 띠 간격은 293 k에서 $2,700{\underline{5}}\;eV$이었던 것이 10K에서는 $2.873{\underline{9}}\;eV$로 변하였다. 광전류 봉우리 위치를 투과단과 비교할 때 293 K에서 30 K까지 관측된 한 개의 봉우리는 가전자대 ${\Gamma}_8$에서 전도대 ${\Gamma}_6$로 전이에 의한 광전류 봉우리이고, 10K에서 관측된 단파장대 417.3 nm($2.971{\underline{4}}\;eV$)의 봉우리는 가전자대 ${\Gamma}_7$에서 전도대 ${\Gamma}_6$로, 431.5 nm($2.873{\underline{3}}\;eV$)의 봉우리는 가전자대 ${\Gamma}_8$에서 전도대 ${\Gamma}_6$로 전이에 의한 광전류 봉우리가 관측된 것으로 판단된다. 광전류 봉우리의 10K에서 단파장대의 가전자대 갈라짐(splitting)에 의해서 측정된 ${\Delta}so$(spin orbit coupling)는 $0.098{\underline{1}}\;eV$ 였다. 10 K에서 광발광 봉우리의 440.7 nm($2.812{\underline{7}}\;eV$)는 자유 엑시톤(free exciton : $E_x$), 443.5 nm ($2.795{\underline{5}}\;eV$)는 주개-얽매인 엑시톤(donor-bound exciton) 인 $I_2(D^0,\;X)$와 445.7 nm ($2.781{\underline{8}}\;eV$)는 반개-얽매인 엑시톤(acceptor-bound exciton) 인 $I_1(A^0,X)$이고, 460.5 nm ($2.692{\underline{3}}\;eV$)는 주개-받개쌍(donor-acceptor pair:DAP) 발광, 580 nm ($2.137{\underline{6}}\;eV$)는 self activated(A)에 기인하는 광발광 봉우리로 분석된다.

• 터널과지하공간
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• 제27권4호
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• pp.243-252
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• 2017

횡등방성 암석의 파괴거동은 등방성 암석의 경우와 큰 차이가 있으므로 횡등방성 암반에 건설되는 암반구조물의 정밀한 안정성 평가를 위해서는 횡등방 파괴함수의 개발이 필요하다. 이 연구에서는 17세기 천문학자 Cassini가 지구둘레를 도는 태양의 궤도를 모델링하기 위해 제안한 Cassini 난형(卵形)곡선을 기반으로 횡등방성 암석의 강도정수 분포함수를 제안하였다. 제안된 강도정수 분포함수는 횡등방성 암석시료에 대한 삼축압축시험을 통해 실험적으로 결정이 가능한 2개의 모델 파라미터로 정의된다. 제안된 강도정수 분포함수를 마찰각과 점착력의 공간분포함수로 채용하여 기존의 Mohr-Coulomb(M-C) 파괴함수를 3차원 횡등방성 M-C 파괴함수로 확장시켰다. 제안된 횡등방성 M-C 파괴함수의 적합성을 검증하기 위해 횡등방성 암석시료의 삼축압축시험 및 진삼축압축시험을 수치모사하였다. 수치실험을 통해 예측된 결과는 실제 실험실 시험에서 관찰되는 횡등방성 암석의 파괴거동과 부합하였다. 또한 진삼축압축시험 수치모사 결과는 암석강도의 중간주응력 의존성이 암석시료에 포함된 미시적 연약면의 공간분포 특성과 밀접한 관련이 있을 수 있음을 보여주었다.