• 한국공작기계학회논문집
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• 제10권6호
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• pp.126-134
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• 2001

Recently, high productivity and cost reduction becomes the most important target of industries due to the worldwide economic competition. One of these efforts is High Speed Machining(HSM), which reduces machining time with the increase of machining speed such as cutting speed and feedrate. It is very important, especially in case that the portion of machining time in production cost is high. This research suggests optimum cutting conditions to reduce cutting time with minimizing term error. For this study, a comprehensive model representing the texture of machining surface is developed, including rubbing phenomenon on the tip of ball end mill and expanded fibbing zone trajectory caused by tool deflection. Experiments show that the suggested set of feed and pick feed is optimum for maintaining the surface roughness identified by rubbing and low cutting speed in minimum.

• 한국항공우주학회지
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• 제37권4호
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• pp.350-358
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• 2009

본 논문은 재진입 비행체의 TAEM 구간 유도와 제어에 관하여 기술 하였다. TAEM 구간은 공기의 밀도와 비행체의 속도의 범위가 큰 특징을 가지고 있으며, 이들 조건하에 TAEM 구간의 유도를 위한 궤적과 비행체의 상태값을 최적화하였다. 최적화된 상태값은 7가지의 상태이며, 상태값은 Down-range, Cross-range, 비행체의 고도, 속도, 경로각, 방위각, 그리고 비행 거리이다. 최적화 연산을 수행하기 위하여 DIDO 프로그램을 사용하였다. 재진입 비행체의 제어를 위하여 인공 신경망을 이용한 되먹임 선형화 제어법을 사용하였다. 비행체의 동역학 모델은 역전파 모델을 통하여 근사화 되고, 근사화된 동역학 모델과 지연된 제어 입력, 플랜트 출력으로부터 새로운 제어 입력을 생성하게 된다. 이를 이용하여 본 논문에서는 앞서 최적화된 7가지의 상태값을 추종하는 결과를 보였다.

• 한국컴퓨터그래픽스학회논문지
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• 제23권5호
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• pp.57-66
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• 2017

본 연구는 물리 기반의 자동차 애니에이션 기술을 연구하였으며, 일반인도 손쉽게 차량 애니에이션을 제작할 수 있도록 직관적인 저작도구를 제안하였다. 사용자가 직접 차량의 이동 경로 및 속도를 지정하면, 이동 경로의 방향적 특성에 기반한 시뮬레이션 구간 분할과 피드백 기반 주행 경로 탐색 기법을 통해 기존 연구보다 빠르고 정확한 주행 시뮬레이션을 수행하도록 하였다. 결과적으로 차선 변경 및 추월을 포함한 단순 주행 애니메이션뿐만 아니라 기존 관련 연구에는 없었던 차량 충돌 애니메이션 또한 제작할 수 있다. 아울러 차체 모델을 실제 차량과 유사하게 설계하였기 때문에, 제동 시 차량이 미세하게 혼들리는 현상이나 추돌 시 차량이 찌그러지는 현상 등 실제에 가까운 차량의 웅직임을 묘사할 수 있다.

• Journal of Astronomy and Space Sciences
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• 제22권4호
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• pp.463-472
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• 2005

본 논문에서는 행성탐사선의 항행해 결정을 위한 동역학 모델을 개발에 대한 내용을 다뤘다. 탐사선이 우주공간을 항행할 때 받는 섭동력으로써, 지구의 비대칭 중력장, 지구의 극축운동, 태양과 달이외의 태양계 행성에 의한 중력, 태양의 의한 상대성효과, 태양복사압 그리고 지구 대기저항에 대한 동역학 모델을 구성하여, 특수섭동론인 코웰 방법에 의거한 탐사선의 궤적 전파기를 개발하였다. 힘 또는 가속도 항으로 표현되는 탐사선의 운동방정식은 아담스 코웰 11차 예측자-수정자 방법에 의해 수치 적분된다. 구성된 전파기를 이용하여 2003년 발사된 화성탐사선인 Mars Express의 실제 임무설계에 사용된 초기궤적요소를 기준으로 임무 궤적을 산출하여 각 섭동력의 영향을 비교해 보았다 이러한 비교는 항행해 결정 시스템의 구성 시 요구 정밀도에 따라 고려해야할 섭동력의 기준을 제시해 주기 때문이다. 또한, 개발된 동역학 모델의 성능시험을 위해 극성 최소 근접거리에서의 위치와 속도를 계산하여 화성 도착여부를 판단하였다. 모의실험을 통해 탐사선의 위치가 화성 작용권구 내에 도달하며 상대속도가 화성에 대한 탈출속도 미만이므로 화성에 포획됨을 확인하였으며, STK(Satellite Tool Kit)를 이용해 산출된 결과와 비교함으로써 본 연구결과가 행성탐사 임무지원에 적합함을 검증하였다.

• 대한전기학회논문지
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• 제43권4호
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• pp.638-647
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• 1994

This paper describes the real time Hardware-In-the Loop Simulation(HILS) that is an efective tool for design, testing and performance evaluation of the guidanc eflight system. The real time HILS was performed by using a 3-axis flight motion simulator, real time computer, I/O system and flight control system hardware along with the assumed flight trajectory of the guidance flight system. Also, we proved the validity of the real time HILS is the guidance flight system by comparing its simulation results with the software simulation data and telemetry data.

• 한국공작기계학회논문집
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• 제14권2호
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• pp.8-13
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• 2005

This study proposes the construction of 2-3 dimensional attractor system for cutting characteristics evaluation of metals. Also this paper aims to find the optimal cutting conditions of diamond turning machine by measuring surface form and roughness to perform the cutting experiment of metals, which are aluminum, with diamond tool. As well, according to change cutting conditions such as feed rate, using diamond turning machine to perform cutting processing, by measuring cutting force and surface roughness and according to cutting conditions the aluminum about cutting properties. Trajectory changes in the attractor indicated a substantial difference in attractor characteristics. Constructed 2-3 dimensional attractor system in this study can be used for cutting characteristics evaluation of metals.

• 한국정밀공학회지
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• 제20권1호
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• pp.63-69
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• 2003

This study proposes the construction of attractor simulator for cutting characteristics evaluation of non-ferrous metals. Also this paper aims to find the optimal cutting conditions of diamond turning machine by measuring surface form and roughness to perform the cutting experiment of non-ferrous metals, which are aluminum, with diamond tool. As well, according to change cutting conditions such as feed rate, cutting force and surface roughness are measured by tool dynamometer. Trajectory changes in the attractor indicated a substantial difference in fractal characteristics. Constructed attractor in this study can be used for cutting characteristics evaluation of non-ferrous metals

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 2000년도 추계학술대회논문집 - 한국공작기계학회
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• pp.83-89
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• 2000

This paper presents a dynamic modeling and a sliding mode controller for the high-speed / high-accuracy position control system. Selected target system is the wire bonder head assembly which is used in semiconductor assembly process. This system is a reciprocating one around the pivot point that consists of VCM(voice coil motor) as a actuator and transducer horn as a bonding tool. For the modeling elements, the system is divided into electrical circuit, magnetic circuit and mechanical system. Each system is modeled by using the bond graph method and united into the full system. Two major aims are considered in the design of the controller. The first one is that the horn must track the given reference trajectory. The second one is that the controller must be realizable by using the DSP board. Computer simulation and experimental results show that the designed sliding mode controller provides better performance than the PID controller.

• 한국항공운항학회지
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• 제22권3호
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• pp.8-14
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• 2014

Arrival management is a tool which provides efficient flow of traffic and reduces ATC workload by determining aircraft's sequence and schedules while they are in cruise phase. As a decision support tool, arrival management should advise on air traffic control service based on the understanding of human factor of its user, air traffic controller. This paper proposed a prediction model for air traffic controller sequencing strategy by analyzing the historical trajectory data. Statistical analysis is used to find how air traffic controller decides the sequence of aircraft based on the speed difference and the airspace entering time difference of aircraft. Logistic regression was applied for the proposed model and its performance was demonstrated through the comparison of the real operational data.

• 한국측량학회지
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• 제35권5호
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• pp.405-414
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• 2017

Spatial data processing often poses challenges due to the unique characteristics of spatial data and this becomes more complex in spatial big data processing. Some tools have been developed and provided to users; however, they are not common for a regular user. This paper presents a benchmark test between two notable tools of spatial big data processing: GIS Tools for Hadoop and SpatialHadoop. At the same time, a MapReduce application is introduced to be used as a baseline to evaluate the effectiveness of two tools and to derive the impact of number of maps/reduces on the performance. By using these tools and New York taxi trajectory data, we perform a spatial data processing related to filtering the drop-off locations within Manhattan area. Thereby, the performance of these tools is observed with respect to increasing of data size and changing number of worker nodes. The results of this study are as follows 1) GIS Tools for Hadoop automatically creates a Quadtree index in each spatial processing. Therefore, the performance is improved significantly. However, users should be familiar with Java to handle this tool conveniently. 2) SpatialHadoop does not automatically create a spatial index for the data. As a result, its performance is much lower than GIS Tool for Hadoop on a same spatial processing. However, SpatialHadoop achieved the best result in terms of performing a range query. 3) The performance of our MapReduce application has increased four times after changing the number of reduces from 1 to 12.