• Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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• v.18 no.3
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• pp.48-54
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• 2004

We have developed a new experimental driving system in order to make an easier drive experiment of PDP. By using the system, we can design and simulate the timing of the pulse in computer environment. As a result of the designed timing, we are able to program at PLD(Programmable Logic Device) and control high-voltage FET switches. The new system can reduce the time of the pulse compared with the previous logic gate ICs that realizes switching logic through hardware. In addition, it is a much easier way of changing the timing of the pulse due to the change of the driving method. By using the developed driving system we experimented on two different things- First, the realization of ADS Driving Method that run commonly; Second, gray scale realization on the three electrodes AC PDP.

• Proceedings of the SAREK Conference
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• 2008.06a
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• pp.16-21
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• 2008

In order to protect the environment from the refrigerant pollution, the $CO_2$ may be regarded as one of the most attractive alternative refrigerants for an automotive air-conditioning system. Control methods for a $CO_2$ system should be different because of $CO_2$'s unique properties as a refrigerant. Especially, the high-side pressure of a $CO_2$ system should be controlled for the effective operation of the system. High-side pressure algorithms, which were composed of the pressure setpoint algorithm and the pressure setpoint reset algorithm, were developed. Pressure setpoint algorithms, by using a neural network and by using a least square method, were developed and compared. Pressure setpoint reset algorithms, by using a fuzzy logic and by using a proportional logic, were also developed and compared. Simulation results showed that a least square method was more useful than a neural network for the pressure setpoint algorithm. And a proportional logic was more practical than a fuzzy logic for the pressure setpoint reset algorithm.

• Bulletin of the Korean Space Science Society
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• 2003.10a
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• pp.100-100
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• 2003

다목적실용위성 1호의 자세제어는 추력기를 이용한 방법과 반작용 휠을 이용한 방법으로 나눌 수 있다. 추력기를 이용한 방법은 위성이 안전모드에 진입하거나 궤도조정시 이용되며, 정상 운영모드에서 촬영임무를 수행할 때는 반작용 휠을 이용하여 위성의 자세를 제어하고 있다. 자세제어는 제로 모멘텀 바이어스(Zero Momentum Bias)를 이용하여 3축 제어방식을 사용하고 있다. 지구센서(CES, Conical Earth Sensor)와 자이로(Gyro)를 통하여 얻은 자세정보를 이용하여 위성의 탑재컴퓨터에서 제어로직을 수행하면 MDE(Motor Drive Electronic)를 통해 모멘텀을 입력받아 반작용 휠의 회전속도를 변화 시켜 자세제어를 수행한다. 본 논문은 위성의 임무기간 동안 반작용 휠을 이용하여 자세제어를 수행한 결과를 바탕으로 위성의 제로 모멘텀 바이어스를 통한 자세제어계의 변화를 분석하여 향후 연장 임무기간 동안 발생할 수 있는 운영상의 문제점을 확인하고, 이에 대한 조치 방법과 자세제어계의 운영 방안을 제시하고 한다.

• Journal of Internet Computing and Services
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• v.2 no.4
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• pp.1-10
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• 2001

In this paper, we define requirements for call distribution of service control logic in Intelligent Network, Also, we propose call distribution mechanism for every subscriber with different call distribution rates, The call distribution mechanism had been developed as a function of Premium-rate Service in Intelligent Network. Our call distribution mechanism applies to percentage distribution instead of circular or hierarchical distribution. The call distribution mechanism consists of call input. output. call distribution processing logic part, random number generator, and customers database. We propose the practical implementation of a call distribution mechanism and call distribution decision indicating number computation method. We show three methods, the rand() function in C language, microsecond by system clock, and proposed algorithm, to get call distribution decision indicating number. In order to optimal call distribution mechanism, we estimated the results of three methods on occurrence values and the number of occurrences.

• Journal of agriculture & life science
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• v.44 no.4
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• pp.69-77
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• 2010

Fuzzy control is widely used for improving temperature control performance as controlling ventilation in greenhouse because the technique can respond more flexibly to the outside air temperature and wind speed. By pre-studied PID and normal fuzzy control this study was performed to obtain the fundamental data that can be established in better greenhouse ventilation control method. The temperature control error by the simple fuzzy control was $1.2^{\circ}C$. The accumulated operating size of the window and the number of operating were 84% and 13, respectively. These showed equivalent control performance with pre-studied result that control error. The accumulated operating size of the window and the number of operating were 75% and 12, respectively. The proposed fuzzy technique was simple control logic method compared with step and PID control methods, but it showed equivalent performance. Therefore, the proposed simple fuzzy control method could be used in micro controller of small programmable memory size and many applications.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2008.06a
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• pp.273-274
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• 2008

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2012.04a
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• pp.57-58
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• 2012

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2006.05a
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• pp.940-940
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• 2006

• Bulletin of the Korean Space Science Society
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• 2007.10a
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• pp.85.1-85.1
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• 2007

• Proceedings of the Korean Vacuum Society Conference
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• 2013.08a
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• pp.120.1-120.1
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• 2013

우주 궤도환경은 $10^{-5}$ torr 이하의 고진공 및 $100^{\circ}C$의 고온과 $150^{\circ}C$이하의 극저온 환경으로 특징지어지며, 위성체 및 위성체 부품은 이와 같은 우주 궤도환경에서의 성능검증이 필수적이다. 지상에서 이와 같은 환경을 모사하기 위해서는 열진공챔버가 사용되며, 열진공 챔버는 진공배기계와 열제어 시스템으로 구성된다. 특히 위성체 또는 위성부품의 열환경을 모사하기 위해 기체 질소를 이용한 폐회로 열제어 시스템이 사용된다. 폐회로 열제어 시스템은 슈라우드, 극저온 블로워, 히터 등으로 구성이 된다. 열제어 시스템의 신뢰성을 높이기 위해서는 핵심 부품인 극저온 블로워의 이중화가 필요하다. 본 논문에서는 위성체 및 위성체 부품의 열진공 시험에 사용되는 열진공 챔버 열제어 시스템의 핵심인 극저온 블로워의 이중화를 위한 기구 설계 및 제어로직 설계 등이 포함되어 있다.