• 한국통신학회논문지
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• 제35권9B호
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• pp.1416-1427
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• 2010

국내 스마트그리드 관련 기술 수준은 일부 분야를 제외하고 선진국들의 수준에 미치지 못하는 것으로 평가되고있다. 이러한 상황 하에서, 본 연구는 스마트그리드 발전의 필수요소인 관련 IT기술을 조망해보고, 스마트그리드 분야에서의 유망 IT R&D분야를 도출하고자 하는 목적으로 수행되었다. 유망 IT R&D 분야의 도출을 위해 스마트그리드 관련 IT기술들의 경제성, 정책부합성, 기술타당성을 평가하는 2단계의 과정을 거쳤고, 그 결과 (1) 센서, (2) 정보보호, (3) AMI 미들웨어, (4) 전력관리의 4대 분야가 유망 분야로 선정되었다. 이 가운데 센서와 AMI 미들웨어 분야는 경제적으로 타당성이 높은 분야이기 때문에 핵심기술 개발에 집중하여 선도적 제품을 타국가보다 세계시장에 빨리 내놓는 전략(Focusing & First Mover Strategy)이 요구된다. 정보보호 분야에서는 국가 기간산업 차원에서의 전력망 안정성 확보 기술 분야와 전력사용자 측면에서의 개인 기업정보보호 기술 분야로 나누어 R&D를 수행하는 R&D Sharing 전략이 기술개발의 효율성을 증대시킬 수 있겠다. 그리고 전력관리 분야는 한국전력 주도로 관리시스템의 요소기술들을 공동 개발하는 전략적 제휴(Strategic Alliance)가 바람직할 것이다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2009년 춘계학술대회논문집
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• pp.125-129
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• 2009

In this paper automatic 3D wing shape modeling program is introduced. The program is developed in Visual Basic based on Net Framework 3.5 environment by using CATIA COM Library, and it is used together with CATIA system to model 3D wings with or without flaps. With this program users can easily construct wing models by specifying geometry parameters which are usually design variables with the aid of easy-to-use GUI environment, and specifying sectional airfoil data is done either by using analytic shape functions such as NACA series airfoils or by providing input files with point data describing the airfoil shape. When all the input parameters are provided, users can either work further with the model in the CATIA system which would be automatically started by the program or save the resultant model in the format of users choice. Unstructured grid generation program is also briefly described which can make grid generation task for a 3D wing easy and efficient one when used together with the wing modeling program by choosing STL format as the model's output format.

• 대한디지털의료영상학회논문지
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• 제14권1호
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• pp.37-42
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• 2012

Pediatric head and neck phantom, using the rate by focusing distance and grid images, Image J using the Quality Assessment and Dose Area Product compared. X-ray laboratory equipment due to the Philips Digital DIAGNOST a 110 cm FFD set and using ACE Non-grid, focusing distance 110 cm (12 : 1), 140 cm (12 : 1), 180 cm (8 : 1) Focused grid, Acryl Phantom (Fluke Model 76-2 Series Phantom) 15.24 cm, by resolution chart image acquisition, image evaluation program (Image J Ver. 1.4.3.67, USA) imaging experiments were analyzed using. Dose Area Product in the Non Grid 0.028 $mGy{\cdot}cm^2$, focusing distance 110 cm (12 : 1), the 0.129 $mGy{\cdot}cm^2$, 140 cm (12 : 1), the 0.135 $mGy{\cdot}cm^2$, 180 cm (8 : 1) was measured with a 0.110 $mGy{\cdot}cm^2$ Non Grid, focusing distance 110 cm (12 : 1), 140 cm (12 : 1), 180 cm (8 : 1) Image obtained when grid using the image J program focusing distance 110 cm with grid based on the measured SNR and PSNR Non Grid if the SNR the 17.307 dB, PSNR of the 20.002 dB, if the SNR 28.755 dB, PSNR was measured by the 31.451 dB. Image J image analysis through the streets, rather than focusing on grid by the rate that could see an increase in dose. Select the grid by a small dose rate reduction is possible.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2001년도 춘계학술대회 논문집
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• pp.435-438
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• 2001

Reverse engineering technology refers to the process that creates a CAD model of an existing part using measuring devices. Recently, non-contact scanning devices have become more accurate and the speed of data acquisition has increased drastically. However, they generate thousands of points per second and various types of point data. Therefore, it becomes a major issue to handle the huge amount and various types of point data. To generate a CAD model from scanned point data efficiently, these point data should be well arranged through point data handling processes such as data reduction and segmentation. This paper proposes a new point data handling method using 3D grids. The geometric information of a part is extracted from point cloud data by estimating normal values of the points. The non-uniform 3D grids for data reduction and segmentation are generated based on the geometric information. Through these data reduction and segmentation processes, it is possible to create CAD models autmatically and efficiently. The proposed method is applied to two quardric medels and the results are discussed.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 1999년도 추계학술발표대회 논문집
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• pp.272-276
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• 1999

The present paper proposes design and manufacturing methods of the carbon/epoxy square grid structure with near zero-CTE in three geometrical principal directions. Bonding strength of the grid structure is examined for different bonding methods. Numerical examples show that maximum displacement of the composite grid structure is almost zero comparing with that of aluminum grid structure with same dimension under thermal loading.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 1995년도 추계 학술대회논문집
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• pp.82-89
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• 1995

In the present paper, a method of nearly orthogonal grid generation in an arbitrary simply-connected 3D domain will be presented. The method is a new direct and non-iterative scheme based on the concept of the decomposition of the global orthogonal transformation into consecutive mapping of a conformal mapping and an auxiliary orthogonal mapping, which was suggested by King and Leal [4]. In our numerical scheme. Kang and Leal's method is extended from 2D problems to 3D problems while the advantage of the non-iterative algorithm is maintained. The essence of the present mapping method is that an iterative scheme can be avoided by introducing a preliminary step. This preliminary step corresponds to a conformal map and is based on the boundary element method(BEM). This scheme is applied to generate several nearly-orthogonal grid systems which are orthogonal at boundaries.

• Journal of Power Electronics
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• 제11권3호
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• pp.360-368
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• 2011

This paper proposes an active frequency with a positive feedback in the d-q frame anti-islanding method suitable for a robust phase-locked loop (PLL) algorithm using the FFT concept. In general, PLL algorithms for grid-connected PV PCS use d-q transformation and controllers to make zero an imaginary part of the transformed voltage vector. In a real grid system, the grid voltage is not ideal. It may be unbalanced, noisy and have many harmonics. For these reasons, the d-q transformed components do not have a pure DC component. The controller tuning of a PLL algorithm is difficult. The proposed PLL algorithm using the FFT concept can use the strong noise cancelation characteristics of a FFT algorithm without a PI controller. Therefore, the proposed PLL algorithm has no gain-tuning of a PI controller, and it is hardly influenced by voltage drops, phase step changes and harmonics. Islanding prediction is a necessary feature of inverter-based photovoltaic (PV) systems in order to meet the stringent standard requirements for interconnection with an electrical grid. Both passive and active anti-islanding methods exist. Typically, active methods modify a given parameter, which also affects the shape and quality of the grid injected current. In this paper, the active anti-islanding algorithm for a grid-connected PV PCS uses positive feedback control in the d-q frame. The proposed PLL and anti-islanding algorithm are implemented for a 250kW PV PCS. This system has four DC/DC converters each with a 25kW power rating. This is only one-third of the total system power. The experimental results show that the proposed PLL, anti-islanding method and topology demonstrate good performance in a 250kW PV PCS.

• Wind and Structures
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• 제5권2_3_4호
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• pp.379-392
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• 2002

Numerical flow computations around an aeroelastic 3D square cylinder immersed in the turbulent boundary layer are shown. Present computational code can be characterized by three numerical aspects which are 1) the method of artificial compressibility is adopted for the incompressible flow computations, 2) the domain decomposition technique is used to get better grid point distributions, and 3) to achieve the conservation law both in time and space when the flow is computed a with moving and transformed grid, the time derivatives of metrics are evaluated using the time-and-space volume. To provide time-dependant inflow boundary conditions satisfying prescribed time-averaged velocity profiles, a convenient way for generating inflow turbulence is proposed. The square cylinder is modeled as a 4-lumped-mass system and it vibrates with two-degree of freedom of heaving motion. Those blocks which surround the cylinder are deformed according to the cylinder's motion. Vigorous oscillations occur as the vortex shedding frequency approaches cylinder's natural frequencies.

• 대한방사선치료학회지
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• 제26권2호
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• pp.171-176
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• 2014

목 적 : Lung SABR plan 에서 AAA의 calculation grid를 변화시켜 선량변화를 분석하고 그에 따른 영향을 연구하여 적절한 적용 방안에 대해 고찰한다. 대상 및 방법 : 모든 plan에 이용된 4D CT image는 Brilliance Big Bore CT(Philips, Netherlands)에서 촬영되었으며 10 건의 Lung SABR plan($Eclipse^{TM}$ ver 10.0.42, Varian, the USA)에서 anisotropic analytic algorithm (AAA, ver. 10, Varian Medical Systems, Palo Alto, CA, USA)을 이용하여 각각 1.0, 3.0, 5.0 mm의 calculation grid로 계산하였다. 결 과 : 10 건의 Lung SABR plan에서 1.0 mm calculation grid를 사용한 경우 $V_{98}$이 각각 처방선량의 약 $99.5{\pm}1.5%$ 였으며 Dmin이 각각 처방선량의 약 $92.5{\pm}1.5%$ 였고 Homogeneity Index(HI)는 약 $1.0489{\pm}0.0025$로 나타났다. 3.0 mm calculation grid를 사용한 경우 $V_{98}$이 각각 처방선량의 약 $90{\pm}4.5%$였으며, Dmin이 각각 처방선량의 약 $87.5{\pm}3%$ 였고 HI가 약 $1.07{\pm}1$로 나타났다. 5.0 mm calculation grid를 사용한 경우 $V_{98}$이 각각 처방선량의 약 $63{\pm}15%$ 였으며, Dmin이 각각 처방선량의 약 $83{\pm}4%$ 였고 HI가 약 $1.13{\pm}0.2$로 나타났다. 결 론 : 1.0 mm calculation grid의 계산 시간이 3.0 mm, 5.0 mm 보다 오래 걸렸지만 grid의 간격이 좁을수록 상대적으로 작은 PTV를 갖는 plan의 정확성을 향상시키는 것으로 나타났다. 또한 Lung과 같이 비교적 넓게 퍼져 있으며 밀도가 낮은 장기의 작은 PTV를 치료해야 하는 경우에는 1.0 mm의 calculation grid를 사용하는 것이 좋을 것으로 사료된다.

• Ocean Systems Engineering
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• 제7권3호
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• pp.195-223
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• 2017

This paper presents 3D numerical simulations of a Free Standing Hybrid Riser under Vortex Induced Vibration, with prescribed motion on the top to replace the motion of the buoyancy can. The model is calculated using a fully implicit discretization scheme. The flow field around the riser is computed by solving the Navier-Stokes equations numerically. The fluid domain is discretized using the overset grid approach. Grid points in near-wall regions of riser are of high resolution, while far field flow is in relatively coarse grid. Fluid-structure interaction is accomplished by communication between fluid solver and riser motion solver. Simulation is based on previous experimental data. Two cases are studied with different current speeds, where the motion of the buoyancy can is approximated to a 'banana' shape. A fully three-dimensional CFD approach for VIV simulation for a top side moving Riser has been presented. This paper also presents a simulation of a riser connected to a platform under harmonic regular waves.