• 한국군사과학기술학회지
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• 제20권1호
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• pp.137-147
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• 2017

Wartime warship damage rate indicates how much damage of friend warships shall have occurred during naval battles accomplished under specific war operational plans. The wartime damage rate analysis provides the baseline of wartime resources requirements. If wartime damage rate is overestimated, the national finance will get to negative effects because of exceeding the budget for inventory, operation, and maintenance of resources. Otherwise, if wartime damage rate is underestimated, the national defense will lose in the war because of lack of critical resources. In this respect, it is important to estimate the wartime damage rate accurately and reasonably. This paper proposes a systematic procedure to estimate the wartime warship damage rate. The procedure consists of five steps; force analysis, operation plan analysis, input variable definition, simulation modeling, and output analysis. Since the combat simulation model is regarded as the main tool to estimate damage rate, the procedure is focused on the development of model and experiments using the model. A case study with virtual data is performed to demonstrate the effectiveness of the developed procedure.

• 한국군사과학기술학회지
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• 제17권6호
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• pp.868-876
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• 2014

Arleigh Burke(DDG-51) and Sejong warship are AEGIS destroyer of US Navy and Korea Navy. These are designed to make more than 30knots by applying a COGAG(COmbined Gas turbine And Gas turbine) system. However, the gas turbine(LM2500) in this system has a low SFC (Specific Fuel Consumption) when the warship operated low speed. So, many kinds of companies are researching the HED(Hybrid Electric Drive) system to improve this problem. The purpose of this paper is to analyze the HED system and simulate by Sejong warship data. Serveral methods were used for that purpose. More specifically, the equipment modeling are employed for regression analysis by LabVIEW. As a result, it was found that the warship installed HED system could cut their fuel bills by as much as about 80,000,000won per year.

• 한국국방경영분석학회지
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• 제36권1호
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• pp.51-64
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• 2010

본 논문에서는 국내에서 개발한 각 군의 주요 워게임 모델의 VV&A 수행 실태를 조사 분석한다. 이를 기초로 VV&A 활동의 참조 틀로써 VV&A 프레임워크를 제안한다. VV&A 프레임워크는 VV&A 기본모델과 참조모델 그리고 지원도구로 구성된다. VV&A 기본모델은 VV&A 프로세스, 산출 문서와 적용기법으로 구성된다. VV&A 참조모델은 VV&A 활동 유형별 확인사항 목록표, VV&A 수행 수준 분석모델과 VV&A 성숙도 관리 모델로 이루어진다. VV&A 지원도구는 VV&A 산출 문서 작성과 관리를 지원하는 도구이다. 제안하는 VV&A 프레임워크는 VV&A 계획 수립과 실행 시 참고할 수 있다.

• 자원환경지질
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• 제33권1호
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• pp.61-75
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• 2000

Through modeling fault network using thin plate finite element technique in the San Andreas Fault system with slip rate over 1mm/year, as well as elevation, heat flow, earthquakes, geodetic data and crustal thickness, we compare the results with velocity boundary conditions of plate based on the NUVEL-1 plate model and the approximation of deformation in the Great Basin region. The frictional and dislocation creep constants of the crust are calculated to reproduce the observed variations in the maximum depth of seismicity which corresponds to the temperature ranging from $350^{\circ}C$ to $410^{\circ}C$. The rheologic constants are defined by the coefficient of friction on faults, and the apparent activation energy for creep in the lower crust. Two parameters above represent systematic variations in three experiments. The pattern of model indicates that the friction coefficient of major faults is 0.17~0.25. we test whether the weakness of faults is uniform or proportional to net slip. The geologic data show a good agreement when fault weakness is a trend of an additional 30% slip dependent weakening of the San Andreas. The results of study suggest that all weakening is slip dependent. The best models can be explained by the available data with RMS mismatch of as little as 3mm/year, so their predictions can be closely related with seismic hazard estimation, at least along faults where no data are available.

• 한국군사과학기술학회지
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• 제14권5호
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• pp.932-940
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• 2011

This study describes computational simulation results in 2-dimensional and 3-dimensional space concerning large scale gap test(LSGT) by using commercial hydrocode such as AUTODYN and LS-DYNA to analyze the detonation phenomenons of high explosives. To consider the possibilities of LSGT simulation, we used Lee - Tarver reaction rate model of PBX-9404 and Comp-B which were implemented AUTODYN's material library. Also we have tried the diverse numerical schemes such as Lagrangian, Eulerian and ALE(Arbitary Lagrangian Eulerian), SPH(Smoothed Particle Hydrodynamics) in LSGT simulations. After LSGT simulations, we compared the simulation results with published results to verify the LSGT simulations. According to the LSGT simulations, we have concluded as follows. In 2-dimensional and 3-dimensional space, Lagrangian solver provided the most reliable results based on analysis time and accuracy. When using two hydrocodes in 2-dimensional space, the simulation results are almost same except one explosive model. We have verified the modeling method and simulation results of the LSGT by using the commenrcial hydrocode in this study.

• 한국군사과학기술학회지
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• 제18권5호
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• pp.485-491
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• 2015

In this study, the experimental and analytical investigation on structural integrity evaluation of spline shaft of self propelled artillery' generator were carried out. For this work, macro and microstructure fractography of spline shaft were observed. According to the results of the structure analysis and simulation, the shaft was redesigned and optimized. To improve the stiffness and shear stress, the material was changed from the SNCM220 to SNCM439 and surface roughness and protective coating treatment are changed to increase the stress relaxation, respectively. From the result of the torsion test of shaft and accelerated life test of generator, the shaft of a SNCM439 with heat-treatment(Q/T) and electroless nickel plating was superior quality reliability and durability than the others. Therefore, modeling and simulation corresponded well with the experimental result and structural safety was confirmed by generator performing.

• 한국국방경영분석학회지
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• 제36권2호
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• pp.11-24
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• 2010

네트워크 중심전(NCW) 및 효과중심작전(EBO)으로 대표되는 현대 및 미래전에서 포병의 신속하고 정확한 정밀타격능력은 전쟁 승패의 중요한 요인으로 작용될 것이다. 본 연구는 대화력전 및 화력지원간 실제 운용되는 환경 중 갱도포병과 같이 타격제한시간이 있는 포병 표적처리에 관한 연구로 여러 가지 제한사항들을 모형 화하여 표적할당 및 사격순서를 동시에 결정하는 문제이다. 본 연구에서는 시간제약이 있는 포병 표적처리문제에서 사격 제한시간을 만족하면서, 총 사격시간을 최소화하는 수리모형과 유전자 알고리즘을 제시하였다. 소형 문제를 이용한 축소실험으로 본 연구에서 제안하는 수리모형과 유전자 알고리즘의 타당성을 입증하였으며, 대형 문제를 이용한 확대실험에서 유전자 알고리즘으로 근사 최적해를 산출하였다.

• 한국국방경영분석학회지
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• 제36권2호
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• pp.25-37
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• 2010

본 연구는 한반도 연안 해역에서 발생할 수 있는 다양한 작전유형을 바탕으로 소형 고속 함정의 적정 소요를 산출하기 위한 방법론적 접근이다. 이 연구방법은 운용 해역을 단위 경비구역으로 구분하고 구역할당 모형과 군집화 모형 등을 활용하였다. 이는 지금까지 작전 운용 장비의 적정 소요 산정시 선형기법등을 여러 가지 다양한 방법을 통해 검증해온 방법과는 달리, 최적화 기법을 활용한 작전 함정의 소요를 모델링하는 방법을 채택하였다. 이러한 경비구역에서 임무수행이 가능한 소형 고속 함정의 적정 소요는 "소요 최적화 프로세스"를 거쳐 소위 "하이브리드 적정 소요 모형"에 의하여 적정성을 산출, 검증하는 모델링 방법으로 제시하고자 한다.

• 한국군사과학기술학회지
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• 제9권4호
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• pp.97-103
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• 2006

A synthetic infrared image can be effectively utilized in various fields such as the recognition and tracking of targets as long as its quality is good enough to reflect the real situations. One way to improve its quality is to use the reference atmosphere which best describes atmospheric properties of regional areas. The east asian reference atmosphere has been developed to represent atmospheric properties of the east asia including Korean peninsula. However, few research has been conducted to examine the effects of this east asian reference atmosphere on the modeling and simulation. In this regard, this paper analyzes the effects of the east asian reference atmosphere on a synthetic infrared image. The research compares the atmospheric transmittance, the surface temperature, and the radiance obtained by using the east asian reference atmosphere with those of the midlatitude reference atmosphere which has been widely applied in the east asia. The results show that the differences of the atmospheric transmittance, the surface temperature, and the radiance between the east asian reference atmosphere and the midlatitude reference atmosphere are significant especially during the daytime. Therefore, it is recommended to apply the east asian reference atmosphere for generating a synthetic infrared image with targets in the east asia.

• 한국군사과학기술학회지
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• 제17권3호
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• pp.350-357
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• 2014

MRDS is a short range missile/rocket defense system which protects a main battle tank(MBT) from threats at a short range. It is composed of 2 radars, 2 infrared trackers(IRT)s, 1 fire control computer(FCC), 2 launchers and countermeasures. In this paper, the radar and the IRT models based on sensing errors, the FCC model based on filtering errors, the launcher model based on driving errors and the countermeasure model based on flying errors are proposed to analyze the defense performance with the approaching RPG-7 and the moving MBT. The simulation results are presented to evaluate and verify the effectiveness of the proposed method.