• 대한인간공학회지
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• 제31권5호
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• pp.647-655
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• 2012

Objective: The purpose of this study was to confirm difference between angular foot movement time and existing foot Fitts' law predicting times, and to develop the angular foot Fitts' law in the foot tapping task. Background: Existing studies of foot Fitts' law focused on horizontal movement to predict the movement time. However, when driving a car, humans move their foot from the accelerator to the brake with a fixed heel. Therefore, we examined the experiment to measure angular foot movement time in reciprocal foot tapping task and compared to conventional foot Fitts' law predicting time. And, we developed the angular foot Fitts' law. Method: In this study, we compared the angular foot movement time in foot tapping task and the predicted time of four conventional linear foot Fitts' law models - Drury's foot Fitts' law, Drury's ballistic, Hoffmann's ballistic, Hoffmann's visually-controlled. 11 subjects participated in this experiment to get a movement time and three target degrees of 20, 40, and 60 were used. And, conventional models were calculated for the prediction time. To analyze the movement time, linear and arc distance between targets were used for variables of model. Finally, the angular foot Fitts' law was developed from experimental data. Results: The average movement times for each experiment were 412.2ms, 474.9ms, and 526.6ms for the 89mm, 172mm, and 253mm linear distance conditions. The results also showed significant differences in performance time between different angle level. However, all of conventional linear foot Fitts' laws ranged 135.6ms to 401.2ms. On the other hand, the angular foot Fitts' law predicted the angular movement time well. Conclusion: Conventional linear foot Fitts' laws were underestimated and have a limitation to predict the foot movement time in the real task related angular foot movement. Application: This study is useful when considering the human behavior of angular foot movement such as driving or foot input device.

• 한국진공학회:학술대회논문집
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• 한국진공학회 2015년도 제49회 하계 정기학술대회 초록집
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• pp.61.1-61.1
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• 2015

Nanoscale semiconductor plasma processing has become one of the most challenging issues due to the limits of physicochemical fabrication routes with its inherent complexity. The mission of future and emerging plasma processing for development of next generation semiconductor processing is to achieve the ideal nanostructures without abnormal profiles and damages, such as 3D NAND cell array with ultra-high aspect ratio, cylinder capacitors, shallow trench isolation, and 3D logic devices. In spite of significant contributions of research frontiers, these processes are still unveiled due to their inherent complexity of physicochemical behaviors, and gaps in academic research prevent their predictable simulation. To overcome these issues, a Korean plasma consortium began in 2009 with the principal aim to develop a realistic and ultrafast 3D topography simulator of semiconductor plasma processing coupled with zero-D bulk plasma models. In this work, aspects of this computational tool are introduced. The simulator was composed of a multiple 3D level-set based moving algorithm, zero-D bulk plasma module including pulsed plasma processing, a 3D ballistic transport module, and a surface reaction module. The main rate coefficients in bulk and surface reaction models were extracted by molecular simulations or fitting experimental data from several diagnostic tools in an inductively coupled fluorocarbon plasma system. Furthermore, it is well known that realistic ballistic transport is a simulation bottleneck due to the brute-force computation required. In this work, effective parallel computing using graphics processing units was applied to improve the computational performance drastically, so that computer-aided design of these processes is possible due to drastically reduced computational time. Finally, it is demonstrated that 3D feature profile simulations coupled with bulk plasma models can lead to better understanding of abnormal behaviors, such as necking, bowing, etch stops and twisting during high aspect ratio contact hole etch.

• 화약ㆍ발파
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• 제33권1호
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• pp.1-12
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• 2015

본 연구에서는 국내 77개소의 벤치발파 현장을 조사하여 암석의 종류 및 산업별로 발파계수 C값을 설정하였고, 대표적인 산업용 화약류에 대한 실험데이터와 화약류 제조사의 데이터를 이용하여 폭약위력계수 e값을 설정하였다. 그 결과로 발파계수 C값은 화강암 등 대표적으로 조사한 암석 5종에 대한 평균적인 값의 범위가 0.21~0.30이었다. 그리고 석산, 광업 및 건설현장의 산업별로 산출한 발파계수 C값은 각각 평균 0.22, 0.13 및 0.26이었다. 한편, 폭약위력계수 e값은 화약류의 반응에너지, 탄동구포비, 폭발속도 및 Langefors 단위 중량당 강도 등 4가지로 산출하였고, 대표적인 화약류인 일반에멀젼은 1, 고성능에멀젼은 0.9 그리고 ANFO는 1로 산출되었다.

• 대한기계학회논문집A
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• 제40권3호
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• pp.281-288
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• 2016

복합재는 재료 불균질성에 의해 고속 충돌 시 방호성능 자료가 산포한다. 본 연구에서는 다수의 충돌시험으로 복합판재 잔류속도 산포를 확보하고 수치해석으로 예측하는 방법을 정립하였다. 먼저 10개의 동일 시편으로 인장시험을 수행하여 파단변형률 산포를 얻었다. 같은 재료로 제작된 4ply([0/90]s)와 8ply([0/90/0/90]s) GFRP(Glass Fiber Reinforced Plastic) 복합판재에 FSP(Fragment Simulating Projectile) 고속 충돌시험을 동일 조건에서 다수 수행하여 잔류속도 산포를 얻었다. 인장시험에서 얻어진 파단 변형률 분포를 이용하여 수치해석을 수행하였다. 충돌속도는 4ply와 8ply 각각 411.7m/s와 592.5m/s이다. 시험 결과와 비교하여 적절한 잔류속도의 산포를 예측할 수 있었다. 추가적으로 복합판재의 경우 Solid요소 대비 Layered Solid요소로 모델링하면 계산시간이 감소되었다.

• 정보처리학회논문지:컴퓨터 및 통신 시스템
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• 제4권12호
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• pp.399-408
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• 2015

직사화기 사격통제장치에서 최적 설계를 위해서는 특정 오차요소가 명중률에 미치는 영향을 파악해야 한다. 이를 위해 가장 좋은 방법은 이들 오차요소에 대한 민감도 식을 구하는 것이나, 체계가 복잡하면 이를 정량적으로 유도하기가 쉽지 않다. 보통 제한된 운용조건에 대해 수치방법으로 민감도를 계산하며, 지상전투차량 등에서 널리 활용되고 있다. 그러나 이 방법은 다량의 시뮬레이션에 의존해야 하므로, 연산 시간이 많이 소요되고 데이터에 의존하므로, 대공화기와 같이 운용조건이 넓게 변화할 경우 민감도가 어떻게 변화할지 직관적으로 이해하는 데 어려움이 있다. 본 논문은 직사화기 탄도에 대한 닫힌 형태 탄도식을 유도하고, 이 식으로부터 오차요소별로 체계 종합오차에 대한 민감도 식을 유도하고, 이들의 영향을 종합하여 명중률을 계산하는 방법을 보인다. 유도된 민감도 식은 수치적분 방법과 달리 연산처리 시간이 짧으면서도 관련 변수 간 물리적 이해가 쉬워 체계설계 시 다양한 운용조건에 대해 편리하게 활용될 수가 있다. 30미리 탄에 대한 시뮬레이션을 통해 본 논문의 유용성을 보인다.

• 한국정보기술학회논문지
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• 제17권9호
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• pp.91-97
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• 2019

레이더를 사용하여 탄도 미사일의 기두부를 추적할 때, 표적의 주변에 있는 각종 기만체들은 표적을 추적하는 레이더의 자원 관리에 큰 부담을 준다. 이러한 부담을 줄이기 위해서 레이더에 수신된 동적 RCS 신호로부터 탄도 미사일 기두부의 신호를 분리할 수 있어야 한다. 본 논문에서는 이미지에서 직선을 추출하는 알고리즘인 허프 변환 방법을 이용하여, 레이더에 수신된 신호로부터 각각의 표적들의 동적 RCS를 분리하는 방법을 제안한다. 기두부와 기만체의 3차원 CAD 모델을 사용하여 표적들의 미세거동을 구현하였다. 또한 미세거동을 가지는 3차원 CAD로부터 표적의 동적 RCS를 계산하고 제안된 알고리즘을 적용하여 알고리즘의 성능을 검증하였다. 시뮬레이션 결과 제안된 방법은 SNR이 10dB에서 미사일 기두부와 기만체의 신호를 분리할 수 있음을 확인하였다.

• Steel and Composite Structures
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• 제22권4호
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• pp.777-796
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• 2016

In this paper, the behavior of woven E-glass fabric composite laminate was experimentally investigated under quasi-static indentation and high velocity impact by flat-ended, hemispherical, conical (cone angle of $37^{\circ}$ and $90^{\circ}$) and ogival (CRH of 1.5 and 2.5) cylindrical perforators. Moreover, the results are compared in order to explore the possibility of extending quasi-static indentation test results to high velocity impact test results in different characteristics such as perforation mechanisms, performance of perforators, energy absorption, friction force, etc. The effects of perforator nose shape, nose length and nose-shank connection shapes were investigated. The results showed that the quasi-static indentation test has a great ability to predict the high velocity impact behavior of the composite laminates especially in several characteristics such as perforation mechanisms, perforator performance. In both experiments, the highest performance occurs for 2.5 CRH projectile and the lowest is related to blunt projectiles. The results show that sharp perforators indicate lower values of dynamic enhancement factor and the flat-ended perforator represents the maximum dynamic enhancement factor among other perforators. Moreover, damage propagation far more occurred in high velocity impact tests then quasi-static tests. The highest damage area is mostly observed in ballistic limit of each projectile which projectile deviation strongly increases this area.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2003년도 ICCAS
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• pp.1278-1282
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• 2003

A new interacting multiple model (IMM) method using intelligent input estimation (IIE) is proposed to track a maneuvering target. In the proposed method, the acceleration level for each sub-model is determined by IIE-the estimation of the unknown acceleration input by a fuzzy system using the relation between maneuvering filter residual and non-maneuvering one. The genetic algorithm (GA) is utilized to optimize a fuzzy system for a sub-model within a fixed range of acceleration input. Then, multiple models are composed of these fuzzy systems, which are optimized for different ranges of acceleration input. In computer simulation for an incoming ballistic missile, the tracking performance of the proposed method is compared with those of the input estimation (IE) technique and the adaptive interacting multiple model (AIMM) method.

• 한국군사과학기술학회지
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• 제21권5호
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• pp.630-639
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• 2018

This paper proposes the design and implementation of adaptive naval gun fire simulator on a naval combat system. The proposed simulator can log data, analysis logged data, modify the BCU(Ballistic Computing Unit) S/W in real-time, and evaluate gun fire performance to check it satisfy requirement or not. When the simulation result satisfies the requirement, the BCU S/W is installed on onboard system. The simulation results show that similar result with actual naval gun fire reslult.

• 한국지능시스템학회:학술대회논문집
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• 한국퍼지및지능시스템학회 2003년도 추계 학술대회 학술발표 논문집
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• pp.99-102
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• 2003

A new interacting multiple model (IMM) method using genetic algorithm (GA)-based intelligent input estimation(IIE) is proposed to track a maneuvering target. In the proposed method, the acceleration level for each sub-model is determined by IIE-the estimation of the unknown acceleration input by a fuzzy system using the relation between maneuvering filter residual and non-maneuvering one. The GA is utilized to optimize a fuzzy system fur a sub-model within a fixed range of acceleration input. Then, multiple models are composed of these fuzzy systems, which are optimized for different ranges of acceleration input. In computer simulation for an incoming ballistic missile, the tracking performance of the proposed method is compared with those of the input estimation(IE) technique and the adaptive interacting multiple model (AIMM) method.