• Journal of the Institute of Electronics and Information Engineers
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• v.50 no.11
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• pp.165-170
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• 2013

When we build up a 3D model from the given 2D images, linear algorithms are often used to reduce computational cost or for initialization of nonlinear algorithms. However, contemporary linear algorithms have apparently linear structures, but virtually they are implemented using SVD. The SVD is also implemented using numerical analysis algorithms that need initialization. Moreover, solutions using SVD are more difficult to analyze than closed-form solutions. To avoid from such inconvenient numerical analysis algorithms of the contemporary methods and for convenient analysis of solutions, this paper proposes a convenient linear method that produces a closed-form solution.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.25 no.12B
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• pp.2060-2068
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• 2000

이 논문은 선형 송·수신 필터의 메모리와 증폭기의 비선형성에 기인하는, 메모리 있는 비선형 시스템의 인식(identification)과 보상에 대해 다룬다. 이와 같은 비선형 시스템은 메모리가 있는 두 개의 선형 시스템 사이에 메모리 없는 비선형 시스템이 있는 것으로 모델링할 수 있으며, 통계적 경사 근사법(stochastic gradient method)으로 선형 시스템의 필터 계수와, 다항식으로 표현되는 비선형 시스템의 계수를 구한다. 이렇게 모델링 되는 통신 채널은 통계적 경사 근사법과 간접 학습 구조를 사용하여 전치 보상기를 설계함으로써 보상한다. 여기서 제시한 비선형 보상 방법은 특정한 통신 채널 모델이 필요 없으며, 적응적으로도 적용이 가능하다.

• Journal of Navigation and Port Research
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• v.27 no.5
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• pp.487-492
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• 2003

The paper describes on the implementation of marine casualty prediction model that is one of the main part of Korean MArine Casualty FOrecasting System (K-MACFOS). In this work, Cell Distributed Linear-In-the-Parameter (CD-LIP) model is proposed and discussed its usability with comparing Baltic model and revised LIP model. As evaluation results by regression analysis of variance, it is known that the CD-LIP model gives best performance to the marine casualty numerical D/B of the target sea area.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2003.05a
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• pp.60-65
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• 2003

The paper describes on the implementation of marine casualty prediction model that is one of the main part of Marine Casualty Forecasting System (MCFS). In this work, Cell Distributed Linear-In-the Parameter (CD-LIP) model is developed and compared with Baltic model using regression analysis of variance. As comparing, it is known that the proposed CD-LIP model has less residual than the Baltic model and, it gives best performance to the marine casualty numeric D/B of target area.

• Journal of the Korean Society of Fisheries and Ocean Technology
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• v.26 no.1
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• pp.76-80
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• 1990

DC-servomotor acts an important role in robots and manipulatirs. But the precise control of DC-motor is difficult by a using usual linear controller because of the nonlinear characteristics of DC-motor. This study suggests the use of fuzzy controller in the control of DC-servomotor speed. The fuzzy controller is designed from a fuzzy model which can represent nonlinear systems very well. Hence the fuzzy controller is very useful in the control of nonlinear systems such as DC-motor. We construct a fuzzy model of DC-servomotor, design a fuzzy controller from the fuzzy model, and compare that with a linear controller. When we use the fuzzy controller, the static ripples are reduced and the rise time is required 20% less than in using a linear controller.

• Journal of the Earthquake Engineering Society of Korea
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• v.13 no.1
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• pp.35-43
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• 2009

Two types of piloti-type high-rise RC building structures having irregularity in the lower two stories were selected as prototypes, and nonlinear time history analysis was performed using OpenSees to verify the analysis technique and to investigate the seismic capacity of those buildings. One of the buildings studied had a symmetrical moment-resisting frame (BF), while the other had an infilled shear wall in only one of the exterior frames (ESW). A fiber model, consisting of concrete and reinforcing bar represented from the stress-strain relationship, was adapted and used to simulate the nonlinearity of members, and MVLEM (Multi Vertical Linear Element Model) was used to simulate the behavior of the wall. The analytical results simulate the behavior of piloti-type high-rise RC building structures well, including the stiffness and yield force of piloti stories, the rocking behavior of the upper structure and the variation of the axial stiffness of the column due to variation in loading condition. However, MVLEM has a limitation in simulating the abrupt increasing lateral stiffness of a wall, due to the torsional mode behavior of the building. The design force obtained from a nonlinear time history analysis was shown to be about $20{\sim}30%$ smaller than that obtained in the experiment. For this reason, further research is required to match the analytical results with real structures, in order to use nonlinear time history analysis in designing a piloti-type high-rise RC building.

• Proceedings of the Korean Information Science Society Conference
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• 1999.10c
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• pp.48-50
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• 1999

본 논문에서는 비선형 편집기를 위해 구현한 디스크 어레이의 구조[1][2][3]에서 편집할 영상의 특성에 따라 최적의 시스템을 구현하는 방법을 성능 분석에 의해 제시한다. 비선형 편집기를 위한 디스크 어레이는 여러 노드로 구성되어 영상의 종류에 따라 확장성이 용이하며 각 노드는 2개의 SCSI버스에 14개의 디스크가 연결 가능하다. 이러한 구조의 시스템에서 디스크의 개수 및 노드의 수를 이용한 SCSI버스의 성능 분석 모델을 제시한다. 성능 분석은 노드 수 및 디스크의 개수에 따라 SCSI 버스의 대역폭 및 디스크들의 검색 속도 비교 후 느린 부분을 찾도록 한다. 주어진 요구에 맞는 시스템을 설계하기 위해 성능 분석 모델을 이용한 최적의 자원을 갖는 비선형 편집 시스템 구현 방법을 제시하며 이를 이용한 무압축 NTSC 비선형 편집기의 설계 및 구현 예를 보인다.

• Proceedings of the Korean Society of Coastal and Ocean Engineers Conference
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• 1996.10a
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• pp.119-123
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• 1996

파랑성분간의 비선형상호작용에 의한 에너지의 교환은 스펙트럼 파랑에너지 보존방정식의 중요한 원천항(source)의 하나이며 이의 정확한 계산에 관한 연구가 파랑모델에서 중요한 문제로서 제기되어 왔다. 그러나 비선형에너지 전달을 엄밀하게 계산하는데는 많은 시간이 소요되기 때문에 현재 현업에서는 스펙트럼파라메타로서 간략화한 식을 사용하고 있다. 비선형상호작용은 파랑이 발달하고 있는 풍역에서 중요하기 때문에 비대칭 스펙트럼에 대한 비선형상호작용의 파라메터화는 풍속이 급변하는 풍장에서 매우 중요하다. (중략)

• Journal of the Computational Structural Engineering Institute of Korea
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• v.22 no.2
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• pp.189-196
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• 2009

This paper presents the subparametric finite element model formulated by partial-linear layerwise theory for the analysis of laminate composites. The proposed model is based on refined approximations of two dimensional plane for orthotropic thick laminate plate as well as thin case. Three dimensional problem can be reduced to two dimensional case by assuming piecewise linear variation of in-plane displacement and a constant value of out-of-plane displacement across the thickness. The integrals of Legendre polynomials are chosen to define displacement fields and Gauss-Lobatto numerical integration is implemented in order to directly obtain maximum values occurred at the nodal points of each layer without other extrapolation techniques. The validity and characteristics of the proposed model have been tested by using orthotropic multilayered plate problem as compared to the values available in the published references. In this study, the convergence test has been carried out to determine the optimal layer model in terms of central deflection and stresses. Also, the distribution of displacements and stresses across the thickness has been investigated as the number of layer is increased.

• Journal of the Korean Society of Propulsion Engineers
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• v.15 no.6
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• pp.98-106
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• 2011

This paper reviews the state-of-the-art thermoacoustic(TA) modeling techniques and research trend to predict major parameters determining combustion instabilities in lean premixed gas turbine combustors. Linear TA modeling results give us an information on eigenfrequencies and initial growth rate of the instabilities. For the prediction, linear relation equation between acoustic waves and heat release oscillations should be derived in the determined system. Key information for this analysis is to determine the heat release fluctuations in the combustor, which is typically obtained by using n-${\tau}$ function from flame transfer function measurements and/or predictions. Great advancement in the linear TA modeling has been made over a couple of decades, and some successful prediction results have been reported in actual gas turbine combustors. However nonlinear TA model developments which are required to analyze nonlinear system behaviors such as limit cycle saturation and transition phenomena are still limited in a very simple system. In order to fully understand combustion instabilities in a complicated real system, nonlinear flame dynamics and acoustic wave interaction with nonlinear system boundary conditions should be explained from the nonlinear TA model developments.