• 한국통신학회논문지
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• 제38A권12호
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• pp.1069-1078
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• 2013

본 논문에서는 최근 차세대 무선 통신네트워크 기술로 주목받고 있는 OFDMA 무선 메쉬통신시스템에서의 분산 시간동기화 기법을 제안한다. 제안방식은 물리계층 기반에서 이루어지는 생체모방 알고리즘을 활용한 자가 분산 시간동기화 기법으로, 인접 이웃노드로부터 수신된 신호의 TDoA(Time Difference of Arrival) 정보를 이용하여 다음 주기의 전송주기와 FFT 시작점을 업데이트한다. 분산처리가 가능한 생체모방 알고리즘의 장점이 반영되어, 제안된 동기화 기법에서도 중앙제어 없이 주위 정보(local Information)와 각 노드에 의한 분산처리만으로 빠르고 간단하게 노드 간 시간 동기 획득이 가능하다. 제안된 분산 시간 동기화 기법은 모의실험을 통하여 시간동기화 수렴 확률 및 정확도 등의 측면에서 성능을 분석한다.

• 융합보안논문지
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• 제21권1호
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• pp.121-127
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• 2021

무선 노드 외에 어떠한 인프라도 존재하지 않는 MANET은 빠른 네트워크 구성할 수 있는 장점을 가지고 있다. 하지만 노드들의 이동, 무선 매체 등은 MANET이 가지고 있는 보안 취약점의 원인이기도 하다. 특히 네트워크상에 존재하는 공격 노드들에 의한 그 피해는 다른 네트워크에 비해 상당히 크다. 따라서 공격노드들에 대한 탐지 기법과 공격으로 인한 피해를 줄이는 기법도 반드시 필요하다. 본 논문에서는 침입탐지의 효율성을 높이기 위한 계층구조 기법과 공격으로 인한 피해를 줄이기 위해 P2P 메시 네트워크 구성 기법을 적용한 협업 기반 침입탐지 기법을 제안하였다. 제안한 기법에서는 클러스터내 노드들에 대한 신뢰도 평가를 통해 사전에 공격 노드에 대한 네트워크 참여를 배제하였다. 그리고 공격 노드에 의한 공격이 탐지되면 클러스터 헤드간의 P2P 메시 네트워크를 통해 네트워크 전역에 공격 노드 정보를 빠르게 전달함으로써 공격 노드의 피해를 최소화하는 방법을 적용하였다. 제안한 기법의 성능 평가를 위해 ns-2 시뮬레이터를 이용하였으며, 비교 실험을 통해 제안한 기법의 우수한 성능을 확인할 수 있었다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제12권1호
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• pp.988-995
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• 2020

Air gun shock systems are commonly used as alternative explosion energy sources for underwater explosion (UNDEX) shock tests owing to their low cost and environmental impact. The airbag inflator of automotive airbag systems is also very useful to generate extremely rapid underwater gas release in labscale tests. To overcome the restrictions on the very small computational time step owing to the very fine fluid mesh around the nozzle hole in the explicit integration algorithm, and also the absence of a commercial solver and software for gas UNDEX of airbag inflator, an idealized airbag inflator and fluid mesh modeling technique was developed using nozzle holes of relatively large size and several small TNT charges instead of gas inside the airbag inflator. The objective of this study is to validate the results of an UNDEX response analysis of one and two idealized airbag inflators by comparison with the results of shock tests in a small water tank. This comparison was performed using the multi-material Arbitrary Lagrangian-Eulerian formulation and fluid-structure interaction algorithm. The number, size, vertical distance from the nozzle outlet, detonation velocity, and lighting times of small TNT charges were determined. Through mesh size convergence tests, the UNDEX response analysis and idealized airbag inflator modeling were validated.

• 한국정보통신학회논문지
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• 제26권9호
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• pp.1272-1278
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• 2022

정부는 2021년 1월에 '중대재해처벌법'을 제정 공포하여, 이 법을 시행하고 있다. 하지만, 2021년 산업재해 사고자수가 전년 동기 대비 10.7% 증가하였다. 따라서, 산업 현장에서는 안전대책이 시급한 현실이다. 본 연구에서는 통신 환경이 열악한 고위험 산업현장의 안전관리를 위하여 BLE Mesh 네트워킹 기술을 적용한다. 복합 센서 AIoT 디바이스로 가스 센싱값, 음성, 모션값을 실시간으로 수집하여, 인공지능 LSTM 알고리즘과 CNN 알고리즘을 통해 정보값을 분석하여 위험 상황을 인식하고, 서버에 전송한다. 서버에서는 전송 받은 위험정보를 실시간으로 모니터링 하여 즉각적인 구호조치가 수행되도록 한다. 본 연구에서 제안하는 AIoT 디바이스와 안전관리 시스템을 고위험군 산업 현장에 적용함으로써, 산업재해를 최소화하고 사회안전망 확대에도 기여할 것이다.

• 한국의학물리학회지:의학물리
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• 제33권4호
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• pp.172-179
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• 2022

Recently, tetrahedral phantoms have been newly adopted as international standard mesh-type reference computational phantoms (MRCPs) by the International Commission on Radiological Protection, and a program has been developed to convert them to computational tomography images and DICOM-RT structure files for application of radiotherapy. Through this program, the use of the tetrahedral standard phantom has become available in clinical practice, but utilization has been difficult due to various library dependencies requiring a lot of time and effort for installation. To overcome this limitation, in this study a newly developed TET2DICOM-GUI, a TET2DICOM program based on a graphical user interface (GUI), was programmed using only the MATLAB language so that it can be used without additional library installation and configuration. The program runs in the same order as TET2DICOM and has been optimized to run on a personal computer in a GUI environment. A tetrahedron-based male international standard human phantom, MRCP-AM, was used to evaluate TET2DICOM-GUI. Conversion into a DICOM-RT dataset applicable in clinical practice in about one hour with a personal computer as a basis was confirmed. Also, the generated DICOM-RT dataset was confirmed to be effectively implemented in the radiotherapy planning system. The program developed in this study is expected to replace actual patient data in future studies.

• International Journal of Aeronautical and Space Sciences
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• 제8권1호
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• pp.95-104
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• 2007

A new design approach of complex geometries such as wing/body configuration is arranged by using overset mesh techniques under large scale computing environment. For an in-depth study of the flow physics and highly accurate design, several special overlapped structured blocks such as collar grid, tip-cap grid, and etc. which are commonly used in refined drag prediction are adopted to consider the applicability of the present design tools to practical problems. Various pre- and post-processing techniques for overset flow analysis and sensitivity analysis are devised or implemented to resolve overset mesh techniques into the design optimization problem based on Gradient Based Optimization Method (GBOM). In the pre-processing, the convergence characteristics of the flow solver and sensitivity analysis are improved by overlap optimization method. Moreover, a new post-processing method, Spline-Boundary Intersecting Grid (S-BIG) scheme, is proposed by considering the ratio of cell area for more refined prediction of aerodynamic coefficients and efficient evaluation of their sensitivities under parallel computing environment. With respect to the sensitivity analysis, discrete adjoint formulations for overset boundary conditions are derived by a full hand-differentiation. A smooth geometric modification on the overlapped surface boundaries and evaluation of grid sensitivities can be performed by mapping from planform coordinate to the surface meshes with Hicks-Henne function. Careful design works for the drag minimization problems of a transonic wing and a wing/body configuration are performed by using the newly-developed and -applied overset mesh techniques. The results from design applications demonstrate the capability of the present design approach successfully.

• 한국콘텐츠학회논문지
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• 제8권5호
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• pp.94-103
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• 2008

본 논문에서는 주어진 3차원 메쉬의 분할에 $\kappa$-평균군집화 기법을 적용한다. 국부적인 최적의 수렴을 피하고 계산시간을 빠르게 하기 위하여 먼저 주어진 메쉬에 대한 첨예정점들을 인지과학적 측면에서 각각 국부적 전역적 기하 특성을 반영하는 곡률과 볼록성을 분석하여 추출한다. 다음에 추출된 첨예정점들은 그들간의 유클리디언 거리대신 측지거리에 기반한 $\kappa$-평균군집화 기법의 반복 수렴으로 $\kappa$ 개의 군집으로 분할된다. $\kappa$-평균군집화의 효과성에 매우 중요한 요인은 적절한 $\kappa$의 초기값을 부여하는 것이다. 따라서 본 논문에서는 $\kappa$의 초기값으로 합리적인 군집 개수를 자동으로 계산한다. 최종적으로 첨예정점들에 속하지 않는 메쉬의 나머지 정점들은 측지거리로 가장 가까이 존재하는 $\kappa$개의 군집에 병합함으로써 메쉬분할이 완성된다.

• Nuclear Engineering and Technology
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• 제51권8호
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• pp.1905-1915
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• 2019

This paper investigated the influence of simple support girds on flow, irrespective of having mixing vanes, in a 1 × 3 array rod bundle by using CFD methodology and the most accurate turbulence model which could reflect the actual physics of the flow was determined. In this context, a CFD model was created simulating the experimental studies on a single-phase flow [1] and the results were compared with the experimental data. In the first part of the study, influence of mesh was examined. Tetra, hybrid and poly type meshes were analyzed and convergence study was carried out on each in order to determine the most appropriate type and density. k - ε Standard and RSM LPS turbulence models were used in this section. In the second part of the study, the most appropriate turbulence model that could reflect the physics of the actual flow was investigated. RANS based turbulence models were examined using the mesh that was determined in the first part. Velocity and turbulence intensity results obtained on the upstream and downstream of the spacer grid at -3d_h, +3d_h and +40d_h locations were compared with the experimental data. In the last section of the study, the behavior of flow through the spacer grid was examined and its prominent aspects were highlighted on the most appropriate turbulence model determined in the second part. Results of the study revealed the importance of mesh type. Hybrid mesh having the largest number of structured elements performed remarkably better than the other two on results. While comparisons of numerical and experimental results showed an overall agreement within all turbulence models, RSM LPS presented better results than the others. Lastly, physical appearance of the flow through spacer grids revealed that springs has more influence on flow than dimples and induces transient flow behaviors. As a result, flow through a simple support grid was examined and the most appropriate turbulence model reflecting the actual physics of the flow was determined.

• 한국멀티미디어학회논문지
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• 제25권4호
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• pp.559-567
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• 2022

The optimal shipping location is determined by measuring the volume and weights of cargo shipped to non-standard cargo carriers. Currently, workers manually measure cargo volume, but automate it to improve work inefficiency. In this paper, we proposed the method of a real-time volume calculation using LiDar sensor for automating cargo measurement of non-standard cargo. For this purpose, we utilized the statistical techniques for data preprocessing and volume calculation, also used Voxel Grid filter to light weighted of data which are appropriate in real-time calculation. We implemented the function of Normal vectors and Triangle Mesh to generate surfaces and Alpha Shapes algorithms to process 3D modeling.

• Wind and Structures
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• 제14권5호
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• pp.435-447
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• 2011

A Computational Fluid Dynamics model is presented in this study for the simulation of the complex fluid flows with free surfaces inside the Tuned Liquid Column Dampers in horizontal motion. The characteristics of the fluid model of the TLCD in horizontal motion include the free surface of the multiphase flow and the horizontal moving frame. In this study, the time depend unsteady Standard ${\kappa}-{\varepsilon}$ turbulent model based on Navier-Stokes equations is chosen. The volume of fluid (VOF) method and sliding mesh technique are adopted to track the free surface of water inside the vertical columns of TLCD and treat the moving boundary of the walls of TLCD in horizontal motion. Several model solution parameters comprising different time steps, mesh sizes, convergence criteria and discretization schemes are examined to establish model parametric independency results. The simulation results are compared with the experimental data in the dimensionless amplitude of the water column in four different configured groups of TLCDs with four different orifice areas. The predicted natural frequencies and the head loss coefficient of TLCDs from CFD model are also compared with the experimental data. The predicted numerical results agree well with the available experimental data.