• 한국자동차공학회논문집
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• 제2권6호
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• pp.94-101
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• 1994

About vibration model of Six-degrees-of-freedom(DOF), in mass load, examined results for knowing dynamic interference and response variation is as follows; In case of putting mass load upon the object, experimented results on two-degrees-of-freedom of the translation-1 direction and the rotation-1 direction at open-loop-control system, about 0.19 arcsed in input of the translation-$0.1{\mu}m$ and $0.022{\mu}m$ on input of the rotation-0.5 arcsec, the justicse of motion equation is acknowledged as confirming the appearance of the interference-$0.022{\mu}m$. In establishing calculation of transformation matrix by using analogue circuit, as simulating results that used incomplete differentiation, interference is $1.7{\times}10^{-3}$ arcsec on input of the translation-$0.1{\mu}m$ and $1.4{\times}10^{4}{\mu}m$ on input of the rotation-0.5 arcsec in open-loop-control system. Also it is $4.2{\times}10^{-4}$ arcsec on input of the translation-$0.1{\mu}m$ and $5.6{\times}10^{-5}{\mu}m$ on input of the rotation-0.5 arcesc in closed-loop-control system. As closed-loop-control system is better than open-loop-control system, equivalent accordance is confirmed on original response. Finally, fundamental validity of this theory is acknowledged.

• 한국정보통신학회논문지
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• 제20권2호
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• pp.335-342
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• 2016

본 논문에서는 고성능 HEVC(High Efficiency Video Coding) 부호기를 위한 루프 내 필터의 효율적인 하드웨어 구조를 제안한다. HEVC는 양자화 에러가 발생하는 복원 영상에서 화질을 향상시키기 위해 디블록킹 필터와 SAO(Sample Adaptive Offset)으로 구성된 루프 내 필터를 사용한다. 그러나 루프 내 필터는 추가적인 연산으로 인하여 부호기와 복호기의 복잡도가 증가되는 원인이 된다. 제안하는 루프 내 필터 하드웨어 구조는 수행 사이클 감소를 위해 디블록킹 필터와 SAO를 3단 파이프라인으로 구현되었다. 또한 제안하는 디블록킹 필터는 6단 파이프라인 구조로 구현되었으며, 효율적인 참조 메모리 구조를 위해 새로운 필터링 순서로 수행된다. 제안하는 SAO는 화소들의 처리를 간소화하며 수행 사이클을 감소시키기 위해 한번에 6개의 화소를 병렬 처리된다. 제안하는 루프 내 필터 하드웨어 구조는 Verilog HDL로 설계되었으며, TSMC $0.13{\mu}m$ CMOS 표준 셀 라이브러리를 사용하여 합성한 결과 약 131K개의 게이트로 구현되었다. 또한 164MHz의 동작 주파수에서 4K@60fps의 실시간 처리가 가능하며, 최대 동작 주파수는 416MHz이다.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 2000년도 봄 학술발표회논문집
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• pp.365-370
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• 2000

A sliding mode fuzzy control (SMFC) algorithm is applied to design a controller for a benchmark problem on a wind- excited building. The structure is a 76-story concrete office tower with a height of 306 meters, hence the wind resistance characteristics are very important for the serviceability as well as the safety. A control system with an active tuned mass damper is assumed to be installed on the top floor. Since the structural acceleration is measured only at ,limited number of locations without measurement of the wind force, the structure of the conventional continuous sliding mode control may have the feed-back loop only. So, an adaptive least mean squares (LMS) filter is employed in the SMFC algorithm to generate a fictitious feed-forward loop. The adaptive LMS filter is designed based on the information of the stochastic characteristics of the wind velocity along the structure. A numerical study is carried out. and the performance of the present SMFC with the ,adaptive LMS filter is investigated in comparison with those of' other control, of algorithms such as linear quadratic Gaussian control, frequency domain optimal control, quadratic stability control, continuous sliding mode control, and H/sub ∞///sub μ/, control, which were reported by other researchers. The effectiveness of the adaptive LMS filter is also examined. The results indicate that the present algorithm is very efficient .

• 대한전기학회논문지:전기기기및에너지변환시스템부문B
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• 제53권3호
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• pp.152-163
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• 2004

This paper presents a sensorless speed control of cylindrical permanent magnet synchronous motors(PMSM) using an adaptive integral binary observer In view of composition with a main loop regulator and an auxiliary loop regulator, the binary observer has a property of the chattering alleviation in the constant boundary layer. However, the steady state estimation accuracy and robustness are dependent upon the width of the constant boundary. In order to improve the steady state performance of the binary observer, the binary observer is formed by adding extra integral dynamics to the switching hyperplane equation. With the help of integral characteristic, the rotor speed can be finely estimated and utilized for a sensorless speed controller for PMSM. Since the Parameters of the dynamic equations such as machine inertia or a viscosity friction coefficient are lot well known, there are many restrictions in the actual implementation. The proposed adaptive integral binary observer applies an adaptive scheme so that observer may overcome the problem caused by using the dynamic equations and the rotor speed is constructed by using the Lyapunov function. The observer structure and its design method are described. The experimental results of the proposed algorithm are presented to demonstrate the effectiveness of the approach.

• Journal of Electrical Engineering and Technology
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• 제4권2호
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• pp.240-248
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• 2009

An approach to control the position for an interior permanent magnet synchronous motor (IPMSM) based on an adaptive integral binary observer is described. The binary controller with a binary observer is composed of a main loop regulator and an auxiliary loop regulator. One of its key features is that it alleviates chatter in the constant boundary layer. However, steady state estimation accuracy and robustness are dependent upon the thickness of the constant boundary layer. In order to improve the steady state performance of the binary observer and eliminate the chattering problem of the constant boundary layer, a new binary observer is formed by adding extra integral dynamics to the existing switching hyperplane equation. Also, the proposed adaptive integral binary observer applies an adaptive scheme because the parameters of the dynamic equations such as the machine inertia and the viscosity friction coefficient are not well known. Furthermore, these values can typically be easily changed during normal operation. However, the proposed observer can overcome the problems caused by using the dynamic equations, and the rotor position estimation is constructed by integrating the rotor speed estimated with a Lyapunov function. Experimental results obtained using the proposed algorithm are presented to demonstrate the effectiveness of the approach.

• Journal of Electrical Engineering and Technology
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• 제5권2호
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• pp.197-208
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• 2010

Unified power flow controller (UPFC) is the most reliable device in the FACTS concept. It has the ability to adjust all three control parameters effective in power flow and voltage stability. In this paper, a linearized model of a power system installed with a UPFC has been presented. UPFC has four control loops that by adding an extra signal to one of them, increases dynamic stability and load angle oscillations are damped. In this paper, after open loop eigenvalue (electro mechanical mode) calculations, state-space equations have been used to design damping controller and it has been considered to influence active and reactive power flow durations as the input of damping controller, in addition to the common speed duration of synchronous generators as input damper signal. To increase stability, further Lead-Lag and LQR controllers, a novel on-line adaptive controller has been used analytically to identify power system parameters. Closed-loop calculations of the electro mechanical mode verify the improvement of system pole placement after controller designing. Suitable operation of adaptive controller to decrease rotor speed oscillations against input mechanical torque disturbances is confirmed by the simulation results.

• 한국경영과학회지
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• 제32권4호
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• pp.1-18
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• 2007

In this paper, we develop an adaptive genetic algorithm (aGA). The aGA has an adaptive scheme which can automatically determine the use of local search technique and adaptively regulate the rates of crossover and mutation operations during its search process. For the adaptive scheme, the ratio of degree of dispersion resulting from the various fitness values of the populations at continuous two generations is considered. For the local search technique, an improved iterative hill climbing method is used and incorporated into genetic algorithm (GA) loop. In order to demonstrate the efficiency of the aGA, i) a canonical GA without any adaptive scheme and ii) several conventional aGAs with various adaptive schemes are also presented. These algorithms, including the aGA, are tested and analyzed each other using various test problems. Numerical results by various measures of performance show that the proposed aGA outperforms the conventional algorithms.

• 대한전자공학회논문지TC
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• 제43권11호
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• pp.141-148
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• 2006

본 논문은 OFDMA 기반의 Wibro 중계국에서 발생되는 루프 간섭 신호의 제거와 위상 보상을 위한 적응 등화기를 사용하여 성능을 개선하기 위한 것이다. Wibro 중계국은 기지국의 통신 가능 영역 확장 및 Throughput 개선을 위하여 사용되는데 송신기와 수신기가 인접해 있으므로 이들간에 루프 간섭의 문제가 성능을 결정하는 중요한 요인이 된다. 논문에서는 먼저 OFDMA 신호를 기저 대역에서 발생시킨 후 Training 시간동안 전송되는 파일롯 톤을 2 가지 삽입 방식으로 조합하여 전송하였다. 또한 부가 잡음 및 루프 간섭 신호에 의한 페이딩파를 발생시켜 수신 신호를 얻은 후 LS (Least Square) 알고리즘을 적용한 채널 추정을 이용을 하여 간섭 신호가 제거된 수신 신호를 복원한 후 적응 등화기를 통과시켜 위상을 보상하였다. 중계기의 성능을 채널 추정 결과, 간섭 제거 후와 등화 출력 신호의 성상도 (Constellation) 및 SNR 변화에 따른 BER 특성 분석을 통하여 개선되었음을 컴퓨터 시뮬레이션을 통해 확인할 수 있었다.

• 한국항공우주학회지
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• 제38권3호
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• pp.228-235
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• 2010

본 논문에서는 틸트로터 항공기의 회전익 모드에 대한 자율비행 유도제어 알고리즘을 적응제어기법을 이용하여 설계하는 것이다. 이를 위해 우선 출력기반 근사적 궤환선형화 기법을 통하여 알고리즘의 내부루프를 구성하고 그로부터 발생하는 모델오차를 단일 은닉층-신경망을 적용하여 상쇄하였다. 그리고 리아푸노프 안정성 이론에 따른 적응제어 갱신법칙은 선형 관측기를 기반으로 설계하였다. 나아가 외부루프는 경로점 유도법칙으로부터 생성되는 궤적을 추종하도록 하였으며 특히 엄밀한 자동착륙 궤적추종 성능 향상을 위하여 방향각 및 비행경로각 시선유도법칙을 설계하였다. 틸트로터 비선형 모델 시뮬레이션 결과는 콜렉티브 입력에서 보이는 순간적인 작동기 포화현상 이외에는 만족할 만한 안정성과 추종성능을 보여 주고 있다.

• 한국항공우주학회지
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• 제42권10호
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• pp.842-850
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• 2014

본 논문은 예측하지 못한 외부 환경 요소 변화로 인해 저하되는 비행 성능을 $L_1$ 적응 제어 기법으로 보상하는 궤적 추종 기법을 제안하였다. 제안된 궤적 추종 기법은 상대 거리를 이용하여 속도 명령을 생성하는 유도 법칙과 속도 명령을 추종하는 적응 제어 루프로 구성되어 있다. 경로 추종 성능을 향상시키기 위하여, 유도 법칙에서 생성한 속도 명령이 적응 제어기의 기준 입력이 되도록 설계하였다. 유도 법칙에서는 목표 궤적과 상대 거리와 그 변화량에 따른 가속도 명령이 생성되며, 이를 적분하여 속도 명령을 생성한다. $L_1$ 적응 제어 루프는 불확실성이 존재하는 환경에서 정밀한 경로 추종 성능을 보장한다. 제안된 경로 추종 시스템은 쿼드로터 항공기를 사용하여 수직 이착륙 및 이동 표적 추종과 같은 비행 실험으로 검증하였다.