• Journal of the Korea Institute of Information and Communication Engineering
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• v.3 no.3
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• pp.639-650
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• 1999

In this paper, a chattering alleviation VSS controller for the sinusoidal type BLDC motor is designed. Dead Zone function is proposed to change the chattering occurring in the transient state from high frequency to low frequency and time-varying gains are applied for the control input to eliminate the steady state excessive chattering in the conventional ISM. The proposed Dead Zone function represents the sliding layer composed of two switching surfaces and if a state vector exists in this layer, the chattering don't occur. Simulation and experimental results confirm the useful effects of the above algorithm.

• Journal of the Korean Society of Propulsion Engineers
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• v.22 no.3
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• pp.28-39
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• 2018

In this study, numerical simulations were performed for steady and unsteady state characteristics of length effects on linear pintle nozzles using the overset grid method. Nozzles and pintles are created separately by an auto grid generation program to use the overset grid method. Appropriate turbulent models and numerical methods are selected for the validation of simulations. Pintle shapes are chosen from five types, with differences in the ratio of length and diameter. The longer the pintle length, the greater the thrust and thrust coefficient. The chamber pressure tendency of steady-state and unsteady-state are different for various pintle velocities. The thrust of the nozzle exit responds to changes in the nozzle throat in the unsteady-state, and the speed of pressure propagation wave generated by movement of the pintle is considered to predict the major factor of performance.

• Asia-pacific Journal of Multimedia Services Convergent with Art, Humanities, and Sociology
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• v.8 no.3
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• pp.571-578
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• 2018

The deteriorated pipline often causes the unexpected leakage and crack. Negligence and late maintenance leads the enormous damage for gas and water resource. This paper proposes early fault detection and diagnosis algorithm for pipeline using acoustic emission (AE) signals. Early fault detection method for pipeline compares the frequency amplitude of the spectrum to that of the spectrum in normal condition. Larger amplitude of the spectrum indicates abnormal condition. Early fault diagnosis algorithm uses support vector machines (SVM), which is trained for normal and abnormal conditions to diagnose the measured AE signal from the target pipeline. In the experiment, a pipeline testbed is constructed similarly to real industrial pipeline. Normal, 5mm cracked, 10mm holed pipelines are installed and tested in this study. The proposed fault detection and diagnosis technique is validated as an efficient approach to detect early faulty condition of pipeline.

• Proceedings of the KIEE Conference
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• 2004.11c
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• pp.650-652
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• 2004

본 논문에서는 간접 벡터 제어 방식의 유도전동기를 위한 하이브리드 퍼지 속도제어기를 설계한다. 제안한 하이브리드 퍼지 속도제어기는 유도 전동기의 속도 응답 성능을 향상시키기 위하여 응답 상태에 따라 PI(비계적분) 제어기와 퍼지 제어기를 선택하여 사용하는 형태이다. 정상상태에서는 PI 제어기를 사용하고 속도 오차값이 크면 퍼지 제어기를 사용한다. 또한 사용된 퍼지 제어기는 퍼지 입력의 파라미터를 튜닝하여 응답 성능을 높였다. 본 논문에서 제안한 하이브리드 퍼지속도 제어기와 기존의 PI 제어기의 성능을 실험을 통하여 비교 검증한다.

• Proceedings of the KIPE Conference
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• 2006.06a
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• pp.13-15
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• 2006

센서리스 제어를 위한 상태 관측기의 설계시 기존의 바이너리 관측기의 성능을 향상시키기 위해 스위칭 평면에 적분항을 추가함으로서 정상상태의 성능을 향상시킬 수 있다. 또한 전동기의 관성계수나 마찰계수와 같은 운동방정식의 파라미터들은 계측하기 어려우며 관측기의 성능저하를 야기하므로 실제구현에서도 많은 제약이 따른다. 이러한 문제를 해결하기 위해 적응 적분바이리 관측기를 제안하다. 그리고 정격속도 이상으로 구동하기 위해서 약계자 영역에서의 센서리스 제안한다. IPMSM이 w가 보다 높은 속도에서 운전되기 위해서는 정격전압이상의 입력이 요구되어진다. 그러나 정격전압에서 d축 전류가 회전자 자속을 감소시키는 방향으로 주입된다면 더 높은 속도에서 운전되어질 수 있다.

• Proceedings of the KIPE Conference
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• 2010.11a
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• pp.64-65
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• 2010

본 논문에서는 250kW급 태양광발전용 인버터에 대한 국내외 기술기준 및 계통연계접속기준에 의한 성능평가방법 및 장비에 대해 소개하고자 한다. 효율, MPPT(maximum power point tracking) 효율 등 정상상태 및 과도상태 성능과 각종 보호기능을 시험할 수 있는 태양전지 및 전력계통 시뮬레이터, 부하장치 등 각종 시험장비의 구성과 시험 방안에 대하여 기술하였으며 국내 기술기준에 의한 시험 결과를 제시하고자 한다.

• Journal of the Korean Society of Propulsion Engineers
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• v.3 no.4
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• pp.93-103
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• 1999

The steady-state performance analysis program for turboprop engine which was used for a small, middle industrial aircraft and a basic trainer aircraft was developed and linear Gas Path Analysis method was applied to Engine Health Monitoring for Turboprop engine. This program was compared with TURBOMARCH program which is well known with performance and power according to flight Mach No. at the standard atmospheric condition to prove a steady-state performance analysis program. From the result, inlet, exit temperature and pressure of each component had error within 3% and especially power according to flight Mach No. had error within 2.4% so that this program could be assured. To make sure if linear Gas Path Analysis is reasonable four cases were selected. The first is the case that fouling is occurred in compressor only. The second is the case that fouling is occurred in compressor and erosion is occurred in turbine. The third is the case that erosion is occurred in both compressor and turbine and power turbine at the same time. Finally, the case that fouling and erosion are occurred in compressor, compressor turbine and power turbine was selected. Different parameters were selected impartially among the independent parameters so that the effect of measurement parameter selection was observed. From the result, the more measurement parameters the smaller RMS error and even though the number of measurement parameters was the same, the RMS error was obtained differently according to which measurement parameters were selected. The case using eight instrument parameters of case IV-4 had small error comparably and was economic and it was important to select optimal number of measurement and optimal measurement parameters.

• Journal of the KSME
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• v.35 no.2
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• pp.154-166
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• 1995

냉동\ulcorner공조기의 성능을 높이기 위해서는 정상상태 운전시는 물론 증발기 열부하 등 각종 작동 조건의 변화에 대응하여 운전의 평형점(balance point) 추이를 적절하게 조정함과 동시에 냉동 사이클 각부의 냉매 상태량을 과도적으로도 제어해야 한다. 이 글에서는 냉동\ulcorner공조기의 자동 제어에 있어서 가장 중요한 요소중의 하나인 냉매계통의 모델화와 냉동 사이클의 응답 및 제어 등에 관해서 서술하고자 한다.

• The Journal of the Acoustical Society of Korea
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• v.17 no.2
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• pp.11-17
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• 1998

본 논문에서는 빠른 수렴 속도를 가지면서 정상 상태에서 작은 오차 레벨을 유지하 는 이중모드 형태의 Stop-and-Go 알고리즘을 제안한다. 제안된 알고리즘은 특별한 결정 영 역을 설정하여 등화기 출력 레벨이 어느 영역에 속하느냐에 따라 MCMA와 판정지향 알고 리즘을 결합한 변형된 Stop-and-Go 알고리즘과 기존의 Stop-and-Go 알고리즘의 동작을 자동 전환한다. 컴퓨터 모의실험 결과, 제안한 알고리즘이 CMA, MCMA 및 Stop-and-Go 알고리즘등과 같은 기존의 적응 블라인드 등화 알고리즘들에 비해 잔류 심볼간 간섭과 정상 상태로의 수렵 속도면에서 모두 우수한 성능을 가짐을 확인하였다.

• Korean Chemical Engineering Research
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• v.46 no.5
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• pp.915-921
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• 2008

In most PEM fuel cell research, effects of cell geometry, physical properties of component such as membrane, carbon cloth, catalyst, etc. and water transport phenomena are key issues. The scope of these research was limited to single cell and stack except BOP(Balance of plant) of fuel cell. The research fouced on the fuel cell system usually neglect to consider detailed transport phenomena in the cell. The research of the fuel cell system was interested in a system performance and system dynamics. In this paper, the effect of the anode recirculation is calculated using the 2D steady-state model. For this work, 2D steady-state modeling and experiments are performed. For convenience of modifying of model equation, not commercial pakage but the in-house algorithm was used in simulation. For an vehicle industry, the analysis of the anode recirculation system helps the optimization of operating condition of the fuel cell.