• Journal of the Korea Academia-Industrial cooperation Society
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• v.14 no.5
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• pp.2092-2099
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• 2013

Through the data transfer race in industry since 1990s, the operational speed of optical disk drive(ODD) becomes commonly over 10,000 rpm. Such high speed operation inevitably causes the vibration, which is also the disturbances in the read-write process of pick-up servo-controller. Generally the vibration disturbance problem can be solved by the vibration isolation using the rubber mount and the increase of robustness of the pick-up servo-controller. Optical disk itself has not been targeted for the vibration reduction, because it is manufactured under the standardized format. In this paper we focused on the increase of critical speed of optical disk, that is, the improvement of dynamic characteristics, with the control of residual stresses which are come from the injection molding process. To do this, first, the residual stresses induced from the injection molding process are calculated using finite element method. The major design parameters of the process conditions are flow rate and melt temperature, which control the residual stresses in optical disk. Second, the critical speed of optical disk is calculated with modal analysis considering residual stress distributions. It was found out that the critical speed can be improved by the control of operational parameters in the injection molding process.

• Aerospace Engineering and Technology
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• v.8 no.2
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• pp.83-91
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• 2009

This paper concerns the dynamic property of TVC system in the upper stage of KSLV-I. The minimum bandwidth of TVC system is predicted by gathering and comparing the dynamic test data through whole development phases of KSLV-I. The linear models which approximate the dynamic data are also suggested. It is shown that the minimum bandwidth of KSLV-I TVC system is guaranteed over 6.0 Hz at one degree command. It is also shown that the linear model of KSLV-I TVC dynamics takes the form of the transfer function with an 8-th order denominator and a 2-nd order numerator. These results will play an important role in analyzing the flight stability and performance of KSLV-I.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.7 no.8
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• pp.1684-1690
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• 2003

In this paper, we proposed a fuzzy controller for the evaluation of the quantization Parameters in the H.263 coder to optimize the subjective quality of each coded frame, keeping the transmission rate constant. We adopted the Mamdani method for fuzzification and the centroid method for defuzzification. The energy and entropy are correlated to features of the HVS in spatial domain, while motion vectors are used to estimate the temporal characteristics of the signal. And then, the fuzzy inputs adapted the variance and the entropy in spatial domain, and the motion vector in temporal domain. We induced the fuzzy membership function and decided the fuzzy relevance to be compatible in visual characteristics. And then, we designed FAM banks. The fuzzy technology has been applied to a practical video compression. This results is obtained an effective rate control technique, an optimum bit allocation and a high subjective quality using fuzzy quantization.

• Proceedings of the KIEE Conference
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• 1997.07f
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• pp.2050-2054
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• 1997

본 논문에서는 직류 대 직류 강압형 변환기의 전달함수 변환에 의한 새로운 제어방법을 제안하였다. 제안된 방법을 외란 및 회로변수 값의 번화 시 나타나는 영향을 최소화시키며, 변환기의 동특성에 영향을 미치는 출력필터의 공진과 동작점 변화에 의한 플랜트 특성 변화를 현저하게 개선시킨다. 먼저 전달함수 변환 제어 시 시스템의 특성을 나타내는 여러 가지 전달함수를 구하여, 이를 기존의 직류 대 직류 변환기에서의 전달 함수와 비교하였다. 또한 외란 및 회로변수 값 변화시의 기준 전압 대 출력 전압 전달함수의 민감도를 구하여 회로변수 값 변화 시 나타나는 특성이 개선됨을 보이고, 마지막으로 모의실험과 실험을 실시하여 제안된 제어 방법이 기존의 제어 방법과 비교하여 우수한 성능을 가짐을 보였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.38 no.12
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• pp.1170-1176
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• 2010

This study addresses adaptive control of UAVs(Unmanned Aerial Vehicles) pitch-axis maneuver. The MRAC(Model Referenced Adaptive Control) approach is employed to accommodate uncertainties which are introduced by feedback linearization of pitch attitude control by elevator input. The model uncertainty is handled by adaptation laws which update model parameters while the UAV is under control by the feedback control law. Steady-state pitch attitude achieved by the stabilizing control law is derived to provide insight on the closed-loop behavior of the controlled system. The proposed idea is free of linearization, gain-scheduling procedures, so that one can design high maneuverability of UAVs for pitching motion in the presence of significant model uncertainty.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.5
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• pp.431-438
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• 2012

Non-linear turbojet engine controller with high operational performance has been designed for the high maneuverability UAV. The turbojet engine dynamic performance code has been developed to reflect the non-linear characteristics on controller design, by which the necessity of non-linear controller design was justified by investigating the limitation of linear model derived from the dynamic performance. The PI-like fuzzy controller was designed and enhanced by combining with conventional derivative control. This designed fuzzy controller proves its effectiveness by showing superior control performances over the conventional PID controller along with guaranteeing the safe operation within compressor surge, flame out and turbine temperature limits etc.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.37 no.4
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• pp.511-519
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• 2013

Switching controllers for active magnetic bearings are claimed to minimize the copper losses because they do not use bias currents. In this study, we compare the performances of the switching controller with those of the widely used proportional-derivative (PD) controller. The PD controller is combined with a synchronous notch filter to reduce the effect of the unbalance disturbance. For a fair and objective comparison, the PD controller is designed systematically. The switching controller is designed so that the dynamics of the two controllers are almost identical. A system model is developed. This model includes the flexible modes of the rotor and the dynamics of the sensors and amplifiers. The simulation results show that the switching controller indeed reduces the copper loss at lower speeds. However, it fails to operate around the speed close to the bending mode of the rotor.

• Nuclear Engineering and Technology
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• v.18 no.2
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• pp.71-77
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• 1986

A one dimensional neutron kinetics program, BIK which is applicable to the safety analyses of PWR's is developed to analyze the reactor core in axial dimension. The BIK employs the finite difference technique in space and $\theta$-time integration method in time. Detailed models for the Doppler and moderator feedbacks and control rod motion are included. The benchmark of the nuclear model is carried out through the ANL benchmark problem and the time dependent nuclear power change in the rod ejection accident of KNU1 is calculated by BIK code. The results indicate that the BIK can predict the neutron dynamics with fair accuracy within the limits of one dimensional analysis and it is useful for the safety analyses of PWR's.

• Journal of the KSME
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• v.32 no.3
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• pp.262-267
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• 1992

이 글은 평면파 소음의 감소 성능을 향상시키고 고차모드로 전달되는 소음의 감소도 가능한 공 조덕트용 능동소음제어장치의 개발에 대하여 논하였으며, 실험결과 개발된 능동소음제어장치의 성능 및 안전성이 기 상품화되어 있는 외국의 제품에 비해 손색없이 뛰어남을 발견하였다. 능 동소음제어장치는 앞으로 고도의 청정, 정숙환경이 요구되는 반도체공장, 방송국 등에 폭넓은 적용이 기대되며, 기존의 흡음처리 대책보다 설치, 보수 및 유지가 간편하다. 특히 덕트내 주요 소음원인 블로워의 소음특성이 저주파 부근에 에너지가 집중되어 있음을 고려할 때 능동소음제 어기술의 공조덕트내 소음제어에의 적용은 매우 효과적이며 경제적일 것으로 기대된다.

• Proceedings of the KIPE Conference
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• 2015.07a
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• pp.67-68
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• 2015

본 논문에서는 멀티모듈 단상 UPS(Uninterruptible Power Supply) 시스템의 예측 제어기법을 제안한다. 제안한 예측 제어기법은 단상 UPS의 수학적 모델링을 통해 설계되었으며, 전류 예측제어를 통해 모드 절환 시 동특성을 향상시켰다. 제안하는 예측 제어기법은 PSIM 시뮬레이션을 통하여 검증하였다.