• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2000년도 하계종합학술대회 논문집(1)
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• pp.115-118
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• 2000

In order to control the flow of traffics in ATM networks and optimize the usage of network resources, an efficient control mechanism is necessary to cope with congestion and prevent the degradation of network performance caused by congestion. To effectively control traffic in UNI(User Network Interface) stage, we proposed algorithm of integrated model using on-line teaming neural network for CAC(Call Admission Control) and UPC(Usage Parameter Control). Simulation results will show that the proposed adaptive algorithm uses of network resources efficiently and satisfies QoS for the various kinds of traffics.

• Structural Engineering and Mechanics
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• 제6권5호
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• pp.529-542
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• 1998

Generalised plane strain solution is presented for simply supported, angle-ply laminated hybrid plate under cylindrical bending. The arbitrary constants in the general solution of the governing differential equations are obtained from the boundary and interface conditions. The response of hybrid plates to sinusoidal loads is obtained to illustrate the effect of the thickness parameter and the ply-angle. The classical lamination theory and the first order shear deformation theory are also assessed.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2004년도 학술대회 논문집 전문대학교육위원
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• pp.126-129
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• 2004

This paper presents the way to analyze the static and dynamic characteristics of the Compound motor and 3 phase slip ring motor using VIS (Virtual Instrument System) and Agilent VEE, GUI(Graphics User Interface) tool. This method is composed of real time measuring of various characteristics, which can't measure using analog meter and analyzer, and presenting and analyzing the static and dynamic characteristics by table, which calculates the measured parameter. Also, this can apply to the various parts.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2003년도 학술회의 논문집 정보 및 제어부문 B
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• pp.886-889
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• 2003

In this paper a design of educational robot based on a PC and/or a microprocessor is discussed. The educational robot has 5 DOF and Is made with Swiss Mini Servomotor and Motor Controller IC LM629N. Also, a GUI(Graphical User Interface) is programmed by Visual Basic. This system is completed to consider control properties of the educational robot with 5-DOF that can be changed the parameter of controller by software.

• 디자인학연구
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• 제20권3호
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• pp.119-128
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• 2007

디지털 기술이 발전하면서 산업디자인 프로세스에 컴퓨터를 활용하는 CAID 필수적인 부분이 되었다. 3차원 모델을 렌더링 하여 사진과 같은 최종 이미지 결과물이 만들어내는 것은 CAID에 특화된 작업들 중 하나이다. 이 작업을 위해 디자이너는 가상 모델의 재질, 조명, 카메라 둥의 위치 및 세부 변수들을 적절히 조절하여야 한다. 기존 CAID도구의 사용자 인터페이스는 이러한 속성을 컴퓨터 그래픽 연산을 위한 변수 설정 창에서 주로 해결하고 있어 디자이너들이 사용하는데 어려움을 겪고 있다. 본 논문에서는 CAID를 위한 디지털 렌더링 작업 특히 라이팅과 관련된 인터페이스 문제를 해결하기 위해 증강현실(Augmented Reality)과 실체적 인터페이스(Tangible Interface)를 활용한 가상의 라이트 조작 도구, TLS(Tangible Lighting Studio)를 제안하였다. 이는 카메라의 위치 설정, 라이팅 효과를 위한 변수설정의 인터페이스를 실체화하고 작업공간에 분산시킴으로써 보다 직관적인 렌더링 작업을 지원하는 도구이다. TLS는 가상의 광원, 카메라, 렌더링 대상 등을 물리적으로 직접 조작할 수 있는 마커, 컨트롤러 유닛들, 사용자가 착용하는 비디오 투시형 HMD 등으로 구성된다. 이를 활용하여 사용자는 증강현실 작업공간에서 직접 라이팅 속성을 조정할 수 있다. 유용성 평가 실험을 통하여 TLS가 기존 CUI(Graphic User Interface)기반 시스템보다 유효성, 효율성 그리고 사용자 만족도가 높다는 점을 발견하였다. TLS는 CAID도구의 인터페이스 분야뿐만 아니라 광원과 카메라의 효과를 활용하는 건축, 사진 촬영 교육 등의 분야에서 효과적으로 활용될 수 있으리라 기대된다.

• 태양에너지
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• 제5권2호
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• pp.11-19
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• 1985

In this paper, the interface stability not to occur mixing and entrainment between the adjacent layers has been studied in the case of the selective withdrawal of a stratum and the injection in stratified fluid formed by the density difference in a small solar pond. There are stability parameter, Richardson number, Rayleigh number and Froude number as the parameters governing stability in order to measure the interface stability on the stratified fluid. The model which could measure the interface stability on the stratified fluid was the small solar pond composed by 1 meters wide, 2 meters high, and 5 meters long. In order to measure the interface stability on the stratified fluid at the inlet port, the middle section and the outlet port, Richardson number, Rayleigh number, and Froude number involved in the parameters governing the stability were calculated by means of the data resulted from the test of the study on hydrodynamic stability between the convective and nonconvective layers in that solar pond. Richardson number written by the ratio of inertia force to buoyancy force can be used in order to measure the stability on the stratified fluid related to the buoyancy force generated from the injection of fluid. Rayleigh number written by the product of Grashof number by Prandtl number can be used in order to measure the stability of the fluid related to the heat flux and diffusivity of viscosity. Froude number written by the ratio of gravity force to inertia force can be used in order to measure the stability of the nonhomogeneous fluid related to the density difference. As the result of calculating the parameters governing stability, the interface stability on the stratified fluid couldn't be identified below the 70cm height from the bottom of the solar pond, but it could be identified above the 70cm height from it at the inlet port, the middle section and the outlet port. When compared with such the three parameters as Richardson number, Rayleigh number, Froude number, the calculated result was in accord with them at inlet port, the middle section and the outlet port. Henceforth, it is learned that even though any of the three parameters is used for the purpose of measuring the interface stability on the stratified fluid, the result will be the same with them. It is concluded that all the use of Richardson number, Rayleigh number, and Froude number, is desirable and infallible to measure the interface stability on the stratified fluid in the case of considering the exist of the fluid flow and the heat flux like the model of the solar pond.

• Advances in aircraft and spacecraft science
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• 제2권2호
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• pp.217-232
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• 2015

To prevent over-testing of the test-item during random vibration testing Scharton proposed and discussed the force limited random vibration testing (FLVT) in a number of publications. Besides the random vibration specification, the total mass and the turn-over frequency of the load (test item), $C^2$ is a very important parameter for FLVT. A number of computational methods to estimate $C^2$ are described in the literature, i.e., the simple and the complex two degrees of freedom system, STDFS and CTDFS, respectively. The motivation of this work is to evaluate the method for the computation of a realistic value of $C^2$ to perform a representative random vibration test based on force limitation, when the adjacent structure (source) description is more or less unknown. Marchand discussed the formal description of getting $C^2$, using the maximum PSD of the acceleration and maximum PSD of the force, both at the interface between load and source. Stevens presented the coupled systems modal approach (CSMA), where simplified asparagus patch models (parallel-oscillator representation) of load and source are connected, consisting of modal effective masses and the spring stiffness's associated with the natural frequencies. When the random acceleration vibration specification is given the CSMA method is suitable to compute the value of the parameter $C^2$. When no mathematical model of the source can be made available, estimations of the value $C^2$ can be find in literature. In this paper a probabilistic mathematical representation of the unknown source is proposed, such that the asparagus patch model of the source can be approximated. The chosen probabilistic design parameters have a uniform distribution. The computation of the value $C^2$ can be done in conjunction with the CSMA method, knowing the apparent mass of the load and the random acceleration specification at the interface between load and source, respectively. Data of two cases available from literature have been analyzed and discussed to get more knowledge about the applicability of the probabilistic method.

• JSTS:Journal of Semiconductor Technology and Science
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• 제10권3호
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• pp.203-212
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• 2010

In this paper, we present an analytical model for the first eigen energy level ($E_0$) of the carriers in the inversion layer in present generation MOSFETs, having ultrathin gate oxides and high substrate doping concentrations. Commonly used approaches to evaluate $E_0$ make either or both of the following two assumptions: one is that the barrier height at the oxide-semiconductor interface is infinite (with the consequence that the wave function at this interface is forced to zero), while the other is the triangular potential well approximation within the semiconductor (resulting in a constant electric field throughout the semiconductor, equal to the surface electric field). Obviously, both these assumptions are wrong, however, in order to correctly account for these two effects, one needs to solve Schrodinger and Poisson equations simultaneously, with the approach turning numerical and computationally intensive. In this work, we have derived a closed-form analytical expression for $E_0$, with due considerations for both the assumptions mentioned above. In order to account for the finite barrier height at the oxide-semiconductor interface, we have used the asymptotic approximations of the Airy function integrals to find the wave functions at the oxide and the semiconductor. Then, by applying the boundary condition at the oxide-semiconductor interface, we developed the model for $E_0$. With regard to the second assumption, we proposed the inclusion of a fitting parameter in the wellknown effective electric field model. The results matched very well with those obtained from Li's model. Another unique contribution of this work is to explicitly account for the finite oxide-semiconductor barrier height, which none of the reported works considered.

• 지구물리와물리탐사
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• 제1권1호
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• pp.19-24
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• 1998

본 논문은 3차원 굴절탄성파 탐사시 얻게 되는 굴절주시를 이용하여 경사진 지층경계면상 속도 분포를 추정하는 방법을 수립코자 수행한 연구를 요약한 것이다. 자료획득은 토모그래피 기법에, 주시 역산은 under-relaxation ART 기법에 의거하였다. 모델은 경사 2층 구조이며, 관련된 매개변수는 지반조사시 만나게 되는 지층을 염두에 두고 선정하였다. 하부 지층에는 수직으로 저속도 혹은 고속도 이상대가 존재하며, 따라서 탐사의 주목적은 이러한 이상대를 탐지하는 것이다. 몇 가지 경우에 대하여 역산을 수행한 결과, 경사 지층 경계면의 경우, 경사 보정을 수행치 않으면 역산 결과는 판독이 어렵거나, 판독하더라도 착오를 일으킬 수 있다는 사실을 확인하였다. 종래 심도 추정을 위한 굴절탄성파 탐사에서, $15^{\circ}$ 이내의 경사지층 경계면을 평균적으로 수평이라고 가정해도 큰 오차가 나지 않는다는 사실을 상기할 때, 앞에 말한 사실은 특이한 일이다.

• 한국전자파학회논문지
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• 제27권12호
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• pp.1084-1096
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• 2016

본 논문에서는 12.5 Gbps의 전송 속도를 갖는 고속 직렬 인터페이스 커넥터(high-speed serial interface connector)의 설계 및 분석 방법을 제안한다. 고속 직렬 인터페이스 커넥터는 다양한 매질로 구성되며, 내부 선로도 복잡한 구조를 가지고 있으므로, 선로의 불연속 부분의 각각을 임피던스 정합하기가 매우 어렵다. 따라서 커넥터의 각 부분을 단순화한 커넥터 라인(connector line)의 구조를 제안하였으며, 이 구조에서 R, L, C, G 파라미터를 추출하고 차동 모드 임피던스를 분석하며, TDT(Time Domain Transmissometry)와 TDR(Time Domain Reflectometry)을 이용하여 임피던스 불연속(impedance discontinuity)을 최소화 하는 방법을 제시한다. 본 논문은 단순화한 커넥터 라인에서 추출된 분석 방법 및 결과를 고속 직렬 인터페이스 커넥터에 적용하였다. 제안한 커넥터는 총 44개의 핀(pin)으로 구성되며, 본 논문에서는 4개의 핀의 폭과 간격을 변경하여 신호 전달 특성을 분석하였다. 분석결과, 접지 핀의 폭이 증가할수록 임피던스는 소폭으로 감소하고, 접지핀과 신호 핀 사이의 간격이 증가할수록 임피던스가 증가했다. 또한, 신호 핀의 폭을 증가시키면 임피던스가 감소하며, 신호 핀과 신호 핀 사이의 간격을 늘리면 임피던스가 증가하였다. 최초 커넥터 임피던스 특성은 $96{\sim}139{\Omega}$ 사이에서 변화되는 값을 나타내었으나, 제안된 커넥터 구조를 적용했을 때 임피던스 특성은 $92.6{\sim}107.5{\Omega}$ 사이의 값으로 나타나, 설계 목표 $100{\Omega}{\pm}10%$를 만족함을 보였다.