• 전자공학회논문지A
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• 제31A권6호
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• pp.199-208
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• 1994

This paper proposes a delay fault test technique for ICs and PCBs with the boundary-scan architectures supporting ANSI/IEEE Std 1149.1-1990. The hybrid delay fault model, which comprises both of gate delay faults and path delay faults, is selected. We developed a procedure for testing delay faults in the circuits with typical boundary scan cells supporting the standard. Analyzing it,we concluded that it is impractical because the test clock must be 2.5 times faster than the system clock with the cell architect-ures following up the state transition of the TAP controller and test instruction set. We modified the boundary-scan cell and developed test instructions and the test procedure. The modified cell and the procedure need test clock two times slower than the system clock and support the ANSI/IEEE standard perfectly. A 4-bit ALU is selected for the circuits under test. and delay tests are simulated by the SILOS simulator. The simulation results ascertain the accurate operation and effectiveeness of the modified mechanism.

• Journal of applied mathematics & informatics
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• 제28권5_6호
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• pp.1315-1322
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• 2010

Let D be a plane domain whose boundary consists of n components and $C_1$, $C_2$ two boundary components of D. We consider the family $F_1$ of conformal mappings f satisfying f(D) $\subset$ {1 < |w| < ${\mu}(f)$}, $f(C_1)=\{|w|=1\}$, $f(C_2)=\{|w|={\mu}(f)\}$. There are conformal mappings $g_0$, $g_1({\in}F_1)$ onto a radial and a circular slit annulus respectively. We obtain the following theorem, $$\{{\mu}(f)|f\;{\in}\;F_1\}=\{\mu|\mu(g_1)\;{\leq}\;{\mu}\;{\leq}\;{\mu}(g_0)\}$$. And we consider the family $F_n$ of conformal mappings $\tilde{f}$ from D onto a covering surfaces of the Riemann sphere satisfying some conditions. We obtain the following theorems, {$\mu|1$ < ${\mu}\;{\leq}\;{\mu}(g_1)$} ${\subset}\;\{{\mu}(\tilde{f})|\tilde{f}\;{\in}\;F_2\}\;{\subset}\;\{{\mu}(\tilde{f})|\tilde{f}\;{\in}\;F_n\}$ and ${\mu}(\tilde{f})\;{\leq}\;{\mu}(g_0)^n$.

• 한국경영과학회:학술대회논문집
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• 대한산업공학회/한국경영과학회 1991년도 춘계공동학술대회 발표논문 및 초록집; 전북대학교, 전주; 26-27 Apr. 1991
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• pp.375-375
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• 1991

• Korean Journal of Mathematics
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• 제22권3호
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• pp.395-406
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• 2014

We study the following nonlinear problem $-div(w(x){\mid}{\nabla}u{\mid}^{p(x)-2}{\nabla}u)+{\mid}u{\mid}^{p(x)-2}u={\lambda}f(x,u)$ in ${\Omega}$ which is subject to Neumann boundary condition. Under suitable conditions on w and f, we give the existence of a positive infimum eigenvalue for the p(x)-Laplacian Neumann problem.

• 대한수학회지
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• 제33권4호
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• pp.857-863
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• 1996

In 1954 M. H. Protter [1] formulated the following boundary value problem as an analogue of the plane Darboux problem.

• 대한의용생체공학회:의공학회지
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• 제10권2호
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• pp.114-116
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• 1989

A method has been proposed for the fully automatic detection of left ventricular endocardial boundary in 2D short axis echocardiogram using geometric model. The procedure has the following three distinct stages. First, the initial center is estimated by the initial center estimation algorithm which is applied to decimated image. Second, the center estimation algorithm is applied to original image and then best-fit elliptic model estimation is processed. Third, best-fit boundary is detected by the cost function which is based on the best-fit elliptic model. The proposed method shows effective result without manual intervention by a human operator.

• 한국측량학회지
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• 제32권spc4_2호
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• pp.375-386
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• 2014

본 연구에서는 지적재조사사업의 완료에 따라 작성할 경계점등록부의 구성방안에 대해 기존의 경계점좌표등록부, 경계점표지등록부, 지상경계점등록부에서 나타난 문제점을 검토하고 이를 바탕으로 경계점의 등록과 관리를 위한 필지경계점 중심의 경계점등록부 작성방안을 제시하였다. 도출된 결과를 요약하면 다음과 같다. 첫째, 3개의 경계점 관련 등록부를 통합하여 관리함으로써 경계점 위치 설명도가 없는 지역에서도 기준점 현황을 바로 확인할 수 있어 신속한 측량이 이루어질 수 있다. 둘째, 일필지 단위의 필지중심이 아닌 필지경계점 중심의 경계점등록부를 작성함으로써 경계점의 연혁관리가 용이하고 경계점의 생성, 이기, 소멸 등에 있어 경계점의 지속적인 관리가 가능하다. 셋째, 경계점 위치 설명도는 토지분할 시점에 작성을 하게 되지만 토지분할의 목적이 주로 건물 신축이므로 건물 준공시점에 경계점 표시변경 신청으로 지형지물과 일치하는 경계점 위치 설명도를 유지할 수 있다.

• 한국멀티미디어학회논문지
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• 제5권3호
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• pp.255-262
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• 2002

윤곽선 시퀀스는 임의 형상을 간단하면서도 정확하게 표현할 수 있는 좋은 표현법이 될 수 있다. 그러나, 형상을 구성하는 화소로부터 쉽게 구할 수 있는 면적, 무게중심, 오리엔테이션 방향, 투영 히스토그램 등과 같은 형상 특징들을 윤곽선 시퀀스로부터 직접 구하기는 어렵기 때문에, 윤곽선 시퀀스를 임의 형상에 대한 표현법으로 잘 사용하지 못하였다. 본 논문에서는 형상 내부의 연속된 화소들로 구성된 수직(또는 수평)의 라인 세그먼트를 의미하는 크로스 섹션 개념을 이용하여, 윤곽선 시퀀스로부터 형상 특징들을 쉽게 구할 수 있음을 보인다. 윤곽선 시퀀스를 한번 순차적으로 탐색함으로써 크로스 섹션을 효율적으로 구할 수 있는 방법을 제안한다. 또한, 이진 영상으로부터 여러 형상의 윤곽선 시퀀스를 자동으로 추출할 수 있는 효율적인 방법도 함께 제안한다. 제안된 방법들은 형상 내부에 홀(hole)이 있는 경우에도 적용할 수 있다. 결과적으로, 윤곽선 시퀀스가 임의 형상 영역에 대한 매우 효과적인 표현이 될 수 있음을 밝힌다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2012년도 춘계학술대회 논문집
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• pp.521-526
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• 2012

It is essential for the accurate time-domain prediction of broadband noise due to turbulence-cascade interaction to develop inflow/outflow boundary conditions to satisfy the following three requirements: to maintain the back ground mean flow, to nonreflect the outgoing disturbances and to generate the specified input gust. The preceding study(1) showed that Perfectly Matched Layer (PML) boundary condition was successfully applied to absorb the outgoing disturbances and to generate the specified gust in the time-domain computations of broadband noise due to interaction of incident gust with a cascade of flat-plates. In present study, PML boundary condition is extended in order to predict steady mean flow that is needed for the computation of noise due to interaction of incident gust with a cascade of airfoils. PML boundary condition is originally designed to absorb flow disturbances superimposed on the steady meanflow in the buffer zone. However, the steady meanflow must be computed before PML boundary condition is applied on the flow computation. In the present paper, PML equations are extended by introducing source term to maintain desired mean flow conditions. The extended boundary condition is applied to the benchmark problem where the meanflow around a cascade of airfoils is predicted. These illustrative computations reveal that the extended PML equations can effectively provide and maintain the target meanflow.

• 한국소음진동공학회논문집
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• 제22권7호
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• pp.685-691
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• 2012

It is essential for the accurate time-domain prediction of broadband noise due to turbulence-cascade interaction to develop inflow/outflow boundary conditions to satisfy the following three requirements: to maintain the back ground mean flow, to nonreflect the outgoing disturbances and to generate the specified input gust. The preceding study showed that perfectly matched layer(PML) boundary condition was successfully applied to absorb the outgoing disturbances and to generate the specified gust in the time-domain computations of broadband noise due to interaction of incident gust with a cascade of flat-plates. In present study, PML boundary condition is extended in order to predict steady mean flow that is needed for the computation of noise due to interaction of incident gust with a cascade of airfoils. PML boundary condition is originally designed to absorb flow disturbances superimposed on the steady meanflow in the buffer zone. However, the steady meanflow must be computed before PML boundary condition is applied on the flow computation. In the present paper, PML equations are extended by introducing source term to maintain desired mean flow conditions. The extended boundary condition is applied to the benchmark problem where the meanflow around a cascade of airfoils is predicted. These illustrative computations reveal that the extended PML equations can effectively provide and maintain the target meanflow.