• Proceedings of the Computational Structural Engineering Institute Conference
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• 2010.04a
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• pp.77-80
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• 2010

최근 건설 프로젝트의 대형화 및 다양한 신공법들의 도입으로 불확실한 위험도 요인들이 점점 증가함으로써 일련의 시스템적 절차에 따른 리스크관리 (Risk Management)체계와 프로젝트 참여자들간의 효율적인 정보전달 방안이 요구되고 있다. 이를 위해 본 연구에서는 '리스크 시각화 시뮬레이션 구축 방법론'을 제시한다. 이는 최근 각종공사 정보 시각화부분에서 주목받고 있는 4D CAD 기술과 리스크 분석을 시스템적인 절차로 구성하여 연계한 방법이다. 시스템적 리스크 분석 절차는 리스크관리기법인 AHP 및 퍼지 분석기법을 동시에 적용하여 합리적인 리스크 정량화를 수행할 수 있도록 구성하였다. 그리고 이로부터 산출된 리스크 요인별 위험정도는 WBS 코드체계 기반으로 4D CAD의 공종과 연계되어 리스크 정도 수준에 따라 설정된 색상으로 시뮬레이션이 구현되도록 구성하였다. 이러한 방법론은 IDEF0 모델링 기법으로 제시함으로써 향후 시스템 구축의 기초 자료로 활용할 수 있도록 하였다.

• Journal of the Korean Society of Propulsion Engineers
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• v.23 no.1
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• pp.101-107
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• 2019

This study conducted a simulation to observe the performance of a multi-turbocharged gasoline internal combustion engine for a high-altitude long-endurance unmanned aerial vehicle (HALE UAV). The WAVE 1-D engine simulation software from Ricardo was used for the engine system modeling and simulation. The specifications of a 2.4-L four cylinder gasoline engine from commercial vehicles and maps of commercial vehicle turbochargers were applied to the multi-stage turbocharged engine system model. Three turbochargers and intercoolers were installed in series for the appropriate intake of pressure for the gasoline engine at a high altitude of 60,000 ft. There was one wastegate for the turbochargers. The operability of the engine system was analyzed via this simulation model.

• Proceedings of the Korean Society of Computer Information Conference
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• 2014.01a
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• pp.439-440
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• 2014

본 논문에서는 기업의 기존 특허 포트폴리오를 비즈니스 모델 컴포넌트의 관점에서 사업타당성 평가를 수행할 수 있는 연구개발 비즈니스 모델링 및 시뮬레이션 시스템을 제안한다. 제안 시스템은 기업이 보유하고 있는 기존 특허들의 기술적 가치를 평가하는 것이 아니라, 비즈니스 모델의 9가지 컴포넌트 관점에서 특허가 보유하고 있는 비즈니스적 특징을 분석할 수 있는 시스템이다. 평가 모델은 4가지 세부 평가모델로 구성하였으며, 시뮬레이션을 수행할 수 있는 기본 파라미터와 제어 파라미터를 제공하여서 파라미터들의 값을 조정하면서 다양한 환경에서의 평가 결과값을 실시간으로 확인할 수 있도록 구현하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.4
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• pp.311-317
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• 2015

This paper describes how to apply one-dimensional simulation to predict unsteady state characteristics of the cold-gas pintle thruster. Mass flow rate, chamber pressure, and nozzle exit pressure are key parameters for thrust control. Chamber pressure rose and fell monotonously with the pintle stroke variation, while thrust variation was different from chamber pressure variation. During the forward pintle stroke operation, the thrust value tended to decrease initially and returned to increase when pintle speed and chamber free volume exceed some specified value. Even though one-dimensional simulation has the limitations to predict unsteady state characteristics, it is still useful for initial performance assessment of various thrusters which adopt an altitude compensation nozzle such as a dual-bell nozzle, prior to experiment or numerical analysis.

• Journal of the Korea Society for Simulation
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• v.31 no.4
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• pp.1-10
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• 2022

This paper describes the development of a modular simulation environment to analyze the performance of guided weapons. For the reusability of the simulation environment, components of the guided weapon simulation are modularized based on MATLAB Simulink. And the module management system is implemented based on Excel and MATLAB GUI for simulation interface and module management. In addition, a method of integration for modules with different interface and a method to set up the guidance and control phase for designing a guided flight scenario are suggested. Finally, to verify the performance of the implemented simulation environment, it was compared with the existing simulation results.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.20 no.4
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• pp.691-697
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• 2016

In this paper, we propose the antenna to appropriate for a UWB communication system, and it meets characteristics for location recognition in predetermined range. Proposed tapered slot antenna was designed through the HFSS simulation tool of Ansys. Inc., it was produced by Taconic TRF-45 based on dielectric constant of 4.5, loss tangent 0.0035, thickness 1.62mm. The tapered slot antenna is analyzed the standing wave ratio and reflection coefficient, radiation pattern in the frequency domain. The impedance bandwidth range of the produced tapered slot antenna is from 3.8 ~ 8.9GHz to 5.1GHz, E-plane and H-plane radiation pattern meet directional antenna characteristics for indoor and outdoor location recognition in predetermined range. The antenna gain is 7.4 dBi(6GHz)in the simulation, the result of measurement demonstrated 7.4 dBi(6 GHz) of antenna maximum gain. Proposed tapered slot antenna meets UWB communication system but simulated and measured results were slightly different.

• Journal of Digital Convergence
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• v.13 no.4
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• pp.303-310
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• 2015

Game technologies are now applied in various engineering areas such as the simulation of surgical operation or the implementation of a cyber model house. One of the essential and important technology in these applications is cutting of the 3D polygon model in real time. Real-time cutting technology is an essential technology needed to implement the simulation of a building demolition or a car assembly for training or educational purpose. Previous cutting method using the conventional BSP-Tree structure has some limitations in that they divide the whole world including the 3D model and its environment, only into two parts with respect to an infinite plane. In this paper, we show a technique cutting the 3D model in a finite extent in order to solve this problem. Specifically, we restricted the cut surface in a finite rectangular area and constructed the mesh for the divided surface. To show the usefulness of our partial cutting technique, an example of the dismantling process simulation of a nuclear reactor polygon model was illustrated.

• Proceedings of the Korea Information Processing Society Conference
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• 2013.11a
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• pp.230-232
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• 2013

본 논문에서는 실내 음영지역에서 사용되는 모바일 와이맥스의 펨토셀 기지국(WFAP; WiMAX Femtocell AP)에 대한 성능을 분석하였다. 시뮬레이션을 통해 와이맥스 펨토셀 기지국의 패킷에러율(PER), Outage, throughput을 확인하였다.

• The Journal of the Acoustical Society of Korea
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• v.4 no.3
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• pp.16-20
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• 1985

압전형 초음파 변환자의 특성을 압전체, matching layer, backing, 매질, tuning 및 구동 회로를 고려하여 해석하였다. 압전체는 KLM 모델을 이용하였고, 모델변수를 실험적으로 추정하여 시뮬레이션 에 대입하였다. 실험적인 RTIL은 면반사에 대한 pulse-echo를 측정하여 계산하였으며, 이론치와 비교할 때 20 dB 주파수 대역내에서 3 dB 이하의 오차가 관찰되었다.

• Journal of Digital Convergence
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• v.15 no.10
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• pp.455-465
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• 2017

This study focuses on design development and verification through virtual simulation based on 3D model data in the cloud platform as a method of utilization of engineering technology of design in the fourth industrial revolution era. The goal of research is to develop and examine a design for the needs of the target that has never been met before through virtual simulations that can be conducted in practice. As a research method, we analyzed secondary data to identify the needs of the target, and did literature research for the ergonomic data and target body development stages. In addition, the design development process of this study was shown meaningful result in design, structure, safety, material, durability through loop test of 7 virtual simulations. This study can be applied to the automated process system based on 3D model data in the 4th industrial revolution era and can be used as an element of the cyber physics system for the additional research.