• Journal of the Korea Society for Simulation
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• v.22 no.2
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• pp.11-19
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• 2013

This paper presents the battle space model, which is capable of propagating various types of emissions from platforms in underwater warfare simulation, predicting interesting encounters between pairs of platforms, and managing environmental information. The battle space model has four components: the logger, spatial encounter predictor (SEP), propagator, and geographic information system (GIS) models. The logger model stores brief data on all the platforms in the simulation, and the GIS model stores and updates environmental factors such as temperature and current speed. The SEP model infers an encounter among the platforms in the simulation, and progresses the simulation to the time when this encounter will happen. The propagator model receives various emissions from platforms and propagates these to other "within-range" platforms by considering the propagation losses and delays. The battle space model is based on the discrete event system specification (DEVS) and the discrete time system specification (DTSS) formalisms. To verify the battle space model, simple underwater warfare between a battleship and a submarine was simulated. The simulation results with the model were the same as the simulation results without the model.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.18 no.1
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• pp.57-62
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• 2014

The benefits of infrastructure support are shown by analyzing a throughput scaling law of an erasure network in which multiple relay stations (RSs) are regularly placed. Based on suitably modeling erasure probabilities under the assumed network, we show our achievable network throughput in the hybrid erasure network. More specifically, we use two types of physical models, a exponential decay model and a polynomial decay model. Then, we analyze our achievable throughput using two existing schemes including multi-hop transmissions with and without help of RSs. Our result indicates that for both physical models, the derived throughput scaling law depends on the number of nodes and the number of RSs.

• Bulletin of the Korean Space Science Society
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• 2003.10a
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• pp.88-88
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• 2003

로켓 엔진 시스템에는 가압가스로 추진제를 엔진으로 공급하는 가압 시스템과 터보펌프를 이용해 엔진으로 고압의 추진제를 공급하는 터보펌프 시스템으로 나눌 수 있으며 터보펌프 시스템은 다시 Gas Generator를 이용하는 개방형 엔진과 Prebumer를 이용한 폐쇄형 엔진인 다단 엔진으로 구분할 수 있다. 로켓의 엔진 시스템은 Turbine, Turbopump, Gas Generator, Thrust Chamber, Tube, Valve, Propellant Tank 등 각 구성품 간에 서로 상호간섭이 매우 심한 공정이다 로켓 엔진 시스템은 이와 같은 상호간섭에 의해 추력 제어 및 혼합비 제어, 추진제 소진 제어 적용 시 정확하고 강인한 제어를 수행하여야 한다. 이를 위해 정확한 동특성 모델을 구축하는 것이 중요하며 모델을 통해 적절한 제어 시스템을 선택하여야 한다. 그러나 현재 국내에는 이에 대한 연구가 미미하며 해외의 경우 로켓은 특수 분야에 속함으로 공개되어 있지 않다. 로켓에 대한 개발 연구에 있어서는 위와 같은 작업이 선행되어야 하며 이에 대한 선행 연구로 한국항공우주연구원에서 Gas Generator를 이용한 개방형 터보펌프 엔진 시스템에 대한 연구를 진행하고 있다. 본 논문에서는 Gas Generator를 이용한 개방형 터보펌프 엔진시스템에 대한 동특성 모델을 구성하였다. 배관부, 터빈, 펌프, 밸브, Gas Generator, 재생냉각, 추력연소실 등 엔진 시스템을 구성하는 구성품에 대한 동특성 모델을 구성하였으며 이를 matlab의 simulink를 통해 각 구성품을 연결하여 최종 엔진시스템의 동특성 모델을 구성하였다. 구성된 동특성 모델을 통해 각종 변화(추진제 밀도 변화, 추력 변화, 혼합비 변화 등)에 대한 엔진 시스템 변화를 예측하여 정확한 엔진 시스템에 대한 이해를 넓혔으며 추력 제어 및 혼합비, 추진제 소진 제어를 최적으로 할 수 있는 제어 시스템 구축을 위한 기초 자료로 이용할 수 있을 것이다.

• The Journal of the Acoustical Society of Korea
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• v.21 no.6
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• pp.510-521
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• 2002

MBE (multi-band excitation) coder can achieve high qualify synthetic speech below 4.0 kbps. There are, however, significant differences of the fine structure between the original spectrum and the synthetic spectrum. They are mainly due to the exclusive partition of voiced and unvoiced regions in frequency domain and the decision procedure based on the experimental threshold. This paper proposes MMBE (mixed multi-band excitation) speech model to overcome drawbacks of a MBE coder. In addition, two analysis methods, which do not need my decision procedure based on a threshold, are presented. Both voiced and unvoiced components can be mixed over all the frequency axis in the MMBE speech model. To illustrate the potential of the proposed speech model, we develop a 2.6 kbps MMBE coder and compare it with a 2.9 kbps MBE coder by both objective and subjective methods. The results have shown that the proposed coder has a better performance even at a lower bit-rate compared with the MBE coder.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.4
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• pp.47-52
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• 2006

Using the equivalent ARMA model representation of the mixed random errors, we propose Klaman filter design methods for aided INS(Inertial Navigation System) which contains the gyroscope mixed random errors. At first step, considering the characteristic of indirect feedback Kalman filter used in the aided INS, we perform the time difference of equivalent ARMA model. Next, according to the order of the time differenced ARMA model, we achieve the state space conversion of that by two methods. If the order of AR part is greater than MA part, we use controllable or observable canonical form. Otherwise, we establish the state apace equation via the method that several step ahead predicts are included in the state variable, where we can derive high and low order models depending on the variable which is compensated from gyroscope output. At final step, we include the state space equation of gyroscope mixed random errors into aided INS Kalman filter model. Through the simulation, we show that both the high and low order filter models proposed give less navigation errors compared to the conventional filter which assume the mixed random errors as white noise.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.1
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• pp.69-75
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• 2009

This paper studies the aerodynamic performance that the vent mixer-new conceptual supersonic mixer-showed with its geometric characteristics. The hole is 2 mm with 2 mm's distance from the wall in case 1 and with no distance in case 2. In case 3 die hole is 1 mm. Case 1 and case 2 showed the same total pressure recovery ratio, of which the case 3 was lower than that. While cases 1-3 had the same reattachment length, the shear layer was thicker in cases 1 and 2 than in case 3. Within the recirculation zone, cases 1 and 2 had lower pressure loss and higher velocity gradient difference than case 3-they enhance mixing between air and fuel. Separation bubble which is developed by the inflow into the recirculation zone has a significant effect on the total pressure recovery ratio in the combustor. Also separation bubble influences pressure distributions and recirculation flows in the recirculation zone. Therefore, inflow rate of air into the recirculation zone mainly affects the performance of vent mixer.

• Journal of Korean Society of Coastal and Ocean Engineers
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• v.1 no.1
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• pp.8-14
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• 1989

A mathematical model for computing the bed friction of combined wave-current flow has been developed based on the Prandtl's mixing length theory. Using various approximate expressions, solutions are obtained explicitly. The computational results are compared and found in reasonable agreements with the data of field measurements.

• Proceedings of the Korean Information Science Society Conference
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• 2001.04a
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• pp.43-45
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• 2001

본 논문에서는 MPEG 비디오 코어 프로파일 디코더 ASIC 상위 구조 설계를 시스템 수준에서 검증하는 기법을 제시한다. 상위 구조 설계는 RISC 프로세서와 펌웨어 그리고 일반 로직이 병존하는 혼합형 구조라는 것과 설계의 상위 단계라는 특징을 가지고 있기 때문에 Verilog HDL과 CSIM 모델 두 가지 모델이 혼합되어 있다. 통합 환경은 C 언어를 이용한 하드웨어 모델링 기법과 PLI를 통한 프로그래밍 언어와 Verilog의 통합 방법을 이용하여 설계 단계에서 각 블록의 특성에 가장 적합한 모델을 이용하여 동작 검증이 가능하도록 하였다.

• Journal of Korea Society of Industrial Information Systems
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• v.21 no.4
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• pp.31-41
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• 2016

This paper is to evaluate the performance of a proposed hybrid genetic algorithm (pro-HGA) approach using closed-loop supply chain (CLSC) model. The proposed CLSC model is a integrated supply chain network model both with forward logistics and reverse logistics. In the proposed CLSC model, the reuse, resale and waste disposal using the returned products are taken into consideration. For implementing the proposed CLSC model, two conventional approaches and the pro-HGA are used in numerical experiment and their performances are compared with each other using various measures of performance. The experimental results show that the pro-HGA approach is more efficient in locating optimal solution than the other competing approaches.

• Korean Chemical Engineering Research
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• v.43 no.3
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• pp.371-379
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• 2005

Adsorption equilibria of the gases $H_2$, $CH_4$, and $C_2H_4$ and their binary mixtures on activated carbon (Calgon co.) have been measured by static volumetric method in the pressure range of 0 to 18 atm at temperatures of 293.15, 303.15, and 313.15 K. From the parameters obtained from single component adsorption isotherm, multi-component adsorption equilibria could be predicted and compared with experimental data. The binary experimental data were applied to four models : extended Langmuir, extended Langmuir-Freundlich, Ideal Adsorbed Solution theory (IAST), and Vacancy Solution Model (VSM). The models were found to describe the experimental data with a reasonable accuracy. Extended L-F model predicts equilibria of mixture better than any other model.