• 실천공학교육논문지
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• 제12권2호
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• pp.309-319
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• 2020

당구는 재미있는 스포츠이지만, 처음 입문한 초심자가 득점 가능한 경로를 계산하고 올바르게 공을 쳐서 보낼 정도로 숙련되기까지의 진입 장벽이 높은 편이다. 당구 초심자가 어느 정도 수준에 도달하기 위해선 지속적인 집중과 훈련을 필요로 하는데, 적절한 동기 부여 요소가 없다면 흥미를 잃어버리기 쉽다. 본 연구는 스테레오 카메라와 VR 헤드셋을 결합한 몰입도 높은 증강 현실 플랫폼 상에서 당구 경로 안내 및 시각 효과를 통해 초심자의 흥미를 유도하고 당구 학습을 가속하는 것을 목표로 두었다. 이를 위해 영상처리를 활용하여 당구공 배치를 인식하고 Unity Engine의 물리 시뮬레이션을 통해 경로 탐색과 시각화를 수행해 실제와 유사한 경로 예측을 구현했다. 이는 당구에 처음 입문하는 초심자가 경로 설계에 대한 부담 없이 공을 올바르게 보내는 훈련에만 집중할 수 있게 만들며, 나아가 오랜 시간 알고리즘이 제안하는 경로를 익힘으로써 점진적으로 당구 숙련도를 높일 수 있다는 점에서 AR 당구의 학습 보조 도구로서의 가능성을 확인할 수 있었다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2005년도 제24회 춘계학술대회논문집
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• pp.219-224
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• 2005

본 연구는 CRW형식 무인항공기 추진시스템의 밸브 작동을 고려한 비행모드에 따른 천이성능특성을 파악하기 위해 SIMULINK를 이용하여 모델링 하였다. 주 엔진시스템의 천이모사에는 ICV 방법이 적용되였다. 그리고 밸브 시스템은 로터리 덕트와 메인 덕트로 빠져나가는 유량을 제어하는 시스템으로서 밸브를 통해 로터리 덕트로 빠져나가는 유량과 메인 덕트를 빠져나가는 유량이 합은 터빈의 출구 유량과 같다는 가정하에 수행 되었으며, 이때 밸브각 변화에 따른 손실, 유량 및 유효 면적 등이 고려되었다. 성능해석은 비행 천이 영역인 고도 1Km 비행 마하수 0.1에서 엔진최대회전수시 회전익 모드에서 고정익 모드로 변환시외 고정익 모드에서 회전익 모드로 변환 경우들이 수행되였다.

• 한국자동차공학회논문집
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• 제16권6호
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• pp.74-80
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• 2008

A combustion of CAI engine is purely dominated by fuel chemical reactions. In order to simulate the combustion of CAI engine, it should be considered the effect of fuel components and chemical kinetics. So it needs enormous computational power. To overcome this problem reduced problem of needing massive computational power, chemical kinetic mechanism and multi-zone method is proposed here in this paper. A reduced chemical kinetic mechanism for a gasoline surrogate was used in this study for a CAI combustion. This gasoline surrogate was modeled as a blend of iso-octane, n-heptane, and toluene. For the analysis of CAI combustion, a multi-zone method as combustion model for a CAI engine was developed and incorporated into the computational fluid dynamics code, STAR-CD, for computing efficiency. This coupled multi-zone model can calculate 3 dimensional computational fluid dynamics and multi-zoned chemical reaction simultaneously in one time step. In other words, every computational cell interacts with the adjacent cells during the chemical reaction process. It can enhance the reality of multi-zone model. A greatly time-saving and yet still relatively accurate CAI combustion simulation model based on the above mentioned two efficient methodologies, is thus proposed.

• 한국항공우주학회지
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• 제50권5호
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• pp.325-332
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• 2022

우주탐사 임무를 수행하기 위해서는 탐사선에 수직이착륙 기능이 필수적으로 탑재되어야 한다. 수직이착륙을 위해서는 탐사선의 엔진이 적절한 추력제어 정확도와 짧은 응답시간을 가져야 한다. 하이브리드 로켓은 이러한 조건을 만족할 수 있는 높은 수준의 추력제어 능력을 갖고 있다. 이 연구는 개발한 하이브리드 로켓 엔진의 추력제어 성능이 수직이착륙에 적절한지 검증하는 것을 목적으로 하고 있다. 이를 위해 가압장치 없이 공급압력이 감소하는 산화제 공급시스템을 적용한 엔진을 사용하여 약 10초 내외의 임무를 수행하고자 하였고, 공급압력 감소가 추력제어 정확도와 응답시간에 미치는 영향을 확인하였다. 실험결과에 의하면 적절한 감소율과 초기 압력 수준이 추력제어 정확도와 응답시간에 중요한 영향을 미치는 인자로 확인되었으며 고도제어 시뮬레이션을 통해 추력제어 성능을 검증했다.

• Journal of Biosystems Engineering
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• 제31권4호
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• pp.342-348
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• 2006

Aerial application using an unmanned agricultural helicopter became necessary for both labor saving and timely spraying. In the previous paper, a rotor system was developed and lift capability was evaluated. The experimental results were compared with simulated predictions using the CFD-ACE program. From the simulation, the relative velocity on the top surface of the blade airfoil increased, resulting in the pressure drop. The CFD analyses were revealed that a drag resistance on the leading edge of the airfoil, a wake at the trailing edge, and a positive pressure underneath the bottom surface were observed. As the results of the simulation, total lifts of 56.8, 74.4 and $95.0kg_f$ were obtained at the 6, 8 and $10^{\circ}$ of AAT (angle of attack), respectively. The simulation results agreed reasonably up to $10^{\circ}$ of AAT. However, at a greater AAT $(<12^{\circ})$ the simulated total lift continuously increased to $105kg_f$, comparing with a decreasing experimental total lift due to the lack of engine power. At a stiff angle of $18^{\circ}$ AAT, a wake was observed at the trailing edge of the airfoil. A rated operating condition determined from the previous paper was also verified through the simulation.

• 대한기계학회논문집
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• 제19권4호
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• pp.1116-1124
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• 1995

Using a cycle simulation program developed by authors, some thermodynamic characteristics of an aircraft ECS under various operating conditions are studied. When the inlet temperature of cockpit and avionics bay, as well as ram air flow, is held fixed, the effect of the change of regulated bleed pressure is examined. When the regulated bleed pressure, and the cockpit and avionics bay inlet temperature are fixed, the effect of the change of ram air flow is also investigated.

• 한국지능시스템학회:학술대회논문집
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• 한국퍼지및지능시스템학회 2003년도 ISIS 2003
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• pp.228-231
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• 2003

This paper presents the leg trajectory generation for the quadruped robot with genetic-fuzzy algorithm. To have the nobility even at uneven terrain, a robot is able to recognize obstacles, and generates moving path of body that can avoid obstacles. This robot should have its own avoidance algorithm against obstacles, forwarding to target without collision. During walking period, n robot recognizes obstacle from external environment with a PSD and some interface, and this obstacle information is converted into proper the body rotation angle by fuzzy inference engine. After this process, we can infer the walking direction and walking distance of body, and finally can generate the optimal Beg trajectory using genetic algorithm. All these methods are verified with PC simulation program, and implemented to SERO-V robot.

• 한국전산유체공학회지
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• 제8권3호
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• pp.56-65
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• 2003

A numerical procedure for analyzing the heat transfer in a regenerative cooling passage of liquid rocket has been developed. The thermal analysis is based on the numerical model of Naraghi〔1〕. The thermodynamic and transport properties of the combustion gases are evaluated using the chemical equilibrium composition. The pressure and heat flux obtained by the isentropic relation are in good agreement with the result of Navier-Stokes equations. The effect of design parameters on heat transfer is addressed for the pressure loss and temperature variation. Also, their constraints in designing the cooling passage are recommended. Finally, in a heated rectangular duct, the effects of secondary flow on heat transfer are scrutinized by the nonlinear k- e -fu of Park et at.〔2〕.

• 오토저널
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• 제14권2호
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• pp.44-53
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• 1992

Automotive transmission is the principle component of vehicle driving system, which transmits the adjusted engine power. The automation of transmission arises from the annoyance of transmission operation such as the frequent stop/start of vehicle and the shifting transients. The study on the optimal shifting condition for the automation of transmission needs the investigation of shifting transients. However, the dynamic modeling theory during transient period is not well-established. In this study, the techniques of dynamic modeling for the power transmission system with Merrite-Wilson gear train are presented. To predict the shifting transients, a driving simulation program is developed, and the results of the analysis are cross-checked in the field test.

• 동력기계공학회지
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• 제6권2호
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• pp.73-81
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• 2002

In this study, electronically controlled automatic transmission adopted on a subcompact model in the market was modelled, and the driving performances of the transmission were simulated with the models. Kinetic and dynamic models of working components are established. The driving simulation program is developed with those models, and the various driving conditions are analyzed. With the results, the dynamic behaviour of the engine and the automatic transmission is easily understood. Especially, the transient performances of torque converter and clutches are deeply analyzed. Skipping the vehicle road test by using this analyzing tool, we can expect the cost down and the reduction of the development period of automatic transmission.