• 한국정보과학회논문지:소프트웨어및응용
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• 제31권3호
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• pp.361-368
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• 2004

본 논문에서는 온라인 학습 자료의 비선형 특징(feature) 추출을 위한 새로운 온라인 비선형 주성분분석(OL-NPCA : On-line Nonlinear Principal Component Analysis) 기법을 제안한다. 비선형 특징 추출을 위한 대표적인 방법으로 커널 주성분방법(Kernel PCA)이 사용되고 있는데 기존의 커널 주성분 분석 방법은 다음과 같은 단점이 있다. 첫째 커널 주성분 분석 방법을 N 개의 학습 자료에 적용할 때 N${\times}$N크기의 커널 행렬의 저장 및 고유벡터를 계산하여야 하는데, N의 크기가 큰 경우에는 수행에 문제가 된다. 두 번째 문제는 새로운 학습 자료의 추가에 의한 고유공간을 새로 계산해야 하는 단점이 있다. OL-NPCA는 이러한 문제점들을 점진적인 고유공간 갱신 기법과 특징 사상 함수에 의해 해결하였다. Toy 데이타와 대용량 데이타에 대한 실험을 통해 OL-NPCA는 다음과 같은 장점을 나타낸다. 첫째 메모리 요구량에 있어 기존의 커널 주성분분석 방법에 비해 상당히 효율적이다. 두 번째 수행 성능에 있어 커널 주성분 분석과 유사한 성능을 나타내었다. 또한 제안된 OL-NPCA 방법은 재학습에 의해 쉽게 성능이 항상 되는 장점을 가지고 있다.

• 한국해양공학회지
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• 제28권5호
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• pp.396-403
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• 2014

This paper considered the prediction of the tension force in the design of a TLP tendon, particularly focusing on the springing problem. Springing is an important parameter that exerts a large tension in special cases. It is a nonlinear phenomenon and requires the 2nd-order wave loads to solve. In this paper, a new prediction method for springing and the resultant extreme tension on the tendon of a TLP is introduced. Using the 2nd-order response function computed using the commercial program WADAM, the probability density function of the 2nd-order tension is obtained from an eigenvalue analysis using a quadratic transfer function and sea spectra. A new method is then suggested to predict the extreme tension loads with respect to the number of occurrences. It is shown that the PDF suggested in this study properly predicts the extreme tension in comparison with the time histories of the 2nd-order tension. The expected tension force is larger than that from a linear analysis in the same time windows. This supports the use of the present method to predict the tension due to springing.

• Structural Engineering and Mechanics
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• 제41권1호
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• pp.113-137
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• 2012

Frame structures with viscoelastic (VE) dampers mounted on them are considered in this paper. It is the aim of this paper to compare the dynamic characteristics of frame structures with VE dampers when the dampers are modelled by means of different models. The classical rheological models, the model with the fractional order derivative, and the complex modulus model are used. A relatively large structure with VE dampers is considered in order to make the results of comparison more representative. The formulae for dissipation energy are derived. The finite element method is used to derive the equations of motion of the structure with dampers and such equations are written in terms of both physical and state-space variables. The solution to motion equations in the frequency domain is given and the dynamic properties of the structure with VE dampers are determined as a solution to the appropriately defined eigenvalue problem. Several conclusions concerning the applicability of a family of models of VE dampers are formulated on the basis of results of an extensive numerical analysis.

• Nuclear Engineering and Technology
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• 제55권6호
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• pp.2172-2194
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• 2023

A variational nodal method (VNM) with unstructured-mesh is presented for solving steady-state and dynamic neutron diffusion equations. Orthogonal polynomials are employed for spatial discretization, and the stiffness confinement method (SCM) is implemented for temporal discretization. Coordinate transformation relations are derived to map unstructured triangular nodes to a standard node. Methods for constructing triangular prism space trial functions and identifying unique nodes are elaborated. Additionally, the partitioned matrix (PM) and generalized partitioned matrix (GPM) methods are proposed to accelerate the within-group and power iterations. Neutron diffusion problems with different fuel assembly geometries validate the method. With less than 5 pcm eigenvalue (k_eff) error and 1% relative power error, the accuracy is comparable to reference methods. In addition, a test case based on the kilowatt heat pipe reactor, KRUSTY, is created, simulated, and evaluated to illustrate the method's precision and geometrical flexibility. The Dodds problem with a step transient perturbation proves that the SCM allows for sufficiently accurate power predictions even with a large time-step of approximately 0.1 s. In addition, combining the PM and GPM results in a speedup ratio of 2-3.

• Transactions on Electrical and Electronic Materials
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• 제18권5호
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• pp.287-297
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• 2017

Novel power system stabilizers (PSSs) have been proposed to effectively dampen low frequency oscillations (LFOs) in multi-machine power systems and have attracted increasing research interest in recent years. Due to this attention, recently, fractional order controllers (FOCs) have found new applications in power system stability issues. Here, a tilt-integral-derivative power system stabilizer (TID-PSS) is proposed to enhance the dynamic stability of a multi-machine power system by providing additional damping to the LFOs. The TID is an extended version of the classical proportional-integral-derivative (PID) applying fractional calculus. The design of the proposed three-parameter tunable TID-PSS is systematized as a nonlinear time domain optimization problem in which the tunable parameters are adjusted concurrently using a modified group search optimization (MGSO) algorithm. An integral of the time multiplied squared error (ITSE) performance index is considered as the objective function. The proposed stabilizer is simulated in the MATLAB/SIMULINK environment using the FOMCON toolbox and the dynamic performance is evaluated on a 3-machine 6-bus power system. The TID-PSS is compared with both classical PID-PSS (PID-PSS) and conventional PSS (CPSS) using eigenvalue analysis and time domain simulations. Sensitivity analyses are performed to assess the robustness of the proposed controller against large changes in system loading conditions and parameters. The results indicate that the proposed TID-PSS provides the better dynamic performance and robustness compared with the PID-PSS and CPSS.

• Earthquakes and Structures
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• 제10권6호
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• pp.1253-1272
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• 2016

For a nonlinear control system, there are many uncertainties, such as the structural model, controlled parameters and external loads. Although the significant progress has been achieved on the robust control of nonlinear systems through some researches on this issue, there are still some limitations, for instance, the complicated solving process, weak conservatism of system, involuted structures and high order of controllers. In this study, the computational structural mechanics and optimal control theory are adopted to address above problems. The induced norm is the eigenvalue problem in structural mechanics, i.e., the elastic stable Euler critical force or eigenfrequency of structural system. The segment mixed energy is introduced with a precise integration and an extended Wittrick-Williams (W-W) induced norm calculation method. This is then incorporated in the market-based control (MBC) theory and combined with the force analogy method (FAM) to solve the MBC robust strategy (R-MBC) of nonlinear systems. Finally, a single-degree-of-freedom (SDOF) system and a 9-stories steel frame structure are analyzed. The results are compared with those calculated by the $H{\infty}$-robust (R-$H{\infty}$) algorithm, and show the induced norm leads to the infinite control output as soon as it reaches the critical value. The R-MBC strategy has a better control effect than the R-$H{\infty}$ algorithm and has the advantage of strong strain capacity and short online computation time. Thus, it can be applied to large complex structures.

• 항공우주시스템공학회지
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• 제16권3호
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• pp.63-72
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• 2022

본 논문에서는 전개형 메쉬 안테나의 동적 강성 설계 및 다물체 동역학을 이용한 요구되는 구동력 및 전개 특성을 분석하고자 한다. 프레임(frame) 요소를 이용하여 전개 구조물을 모델링한다. 다각(polygon) 형상 전개 구조물의 전개/수납된 형상에 따른 고유치 문제를 분석하였다. Kane's 방정식을 이용하여 전개 구조물의 다물체 동역학 방정식을 유도하고 PUTD (pseudo upper triangular decomposition) 방법을 적용하여 구속조건 문제를 해결하였다. 고유진동 해석 및 다물체 동역학 시뮬레이션을 통해 설계된 전개형 구조의 구조 동특성 및 실현성을 살펴보고자 한다.

• Advances in aircraft and spacecraft science
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• 제8권4호
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• pp.345-372
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• 2021

The analysis of nonlinear vibrations, buckling, post-buckling, flutter boundary determination and post-flutter behavior of a homogeneous curved plate assuming cylindrical bending is conducted in this article. Other assumptions include simply-supported boundary conditions, supersonic aerodynamic flow at the top of the plate, constant pressure conditions below the plate, non-viscous flow model (using first- and third-order piston theory), nonlinear structural model with large deformations, and application of mechanical and thermal loads on the curved plate. The analysis is performed with constant environmental indicators (flow density, heat, Reynolds number and Mach number). The material properties (i.e., coefficient of thermal expansion and modulus of elasticity) are temperature-dependent. The equations are derived using the principle of virtual displacement. Furthermore, based on the definitions of virtual work, the potential and kinetic energy of the final relations in the integral form, and the governing nonlinear differential equations are obtained after fractional integration. This problem is solved using two approaches. The frequency analysis and flutter are studied in the first approach by transferring the handle of ordinary differential equations to the state space, calculating the system Jacobin matrix and analyzing the eigenvalue to determine the instability conditions. The second approach discusses the nonlinear frequency analysis and nonlinear flutter using the semi-analytical solution of governing differential equations based on the weighted residual method. The partial differential equations are converted to ordinary differential equations, after which they are solved based on the Runge-Kutta fourth- and fifth-order methods. The comparison between the results of frequency and flutter analysis of curved plate is linearly and nonlinearly performed for the first time. The results show that the plate curvature has a profound impact on the instability boundary of the plate under supersonic aerodynamic loading. The flutter boundary decreases with growing thermal load and increases with growing curvature.

• 대한토목학회논문집
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• 제3권4호
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• pp.95-107
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• 1983

기존(旣存) 범용 구조해석용(構造解析用) 프로그램들은 선택(選擇)된 역학적(力學的) 이론(理論), 계산(計算) algorithm등이 고정(固定)되어 있으므로 이용자(利用者)는 프로그램을 원하는 대로 control하기 어렵고 프로그램에 정의(定義)된 대로 data input만 준비(準備)한다. 이용자(利用者)가 계산과정(計算過程)을 control 할 수 있으며 원하는 역학적(力學的) 이론(理論) 및 계산(計算) algorithm등을 보완(補完)하여 이용(利用)할 수 있도록 한 구조해석용(構造解析用) 프로그램인 Symbolic Manipulation Program들이 개발(開發)되었으나 이들은 single domain 문제(問題) 해석용(解析用)이므로 대형(大型)콤퓨터가 필요(必要)하다. 본(本) 연구(硏究)에서는 substructure technique을 도입(導入)하여 구조물(構造物)을 multi domain으로 하여 중(中), 소형(小型)콤퓨터로도 해석(解析)할 수 있으며, matrix analysis 및 finite element analysis를 할 수 있도록 finite element characteristic arrays(Stiffness, Mass matrix)등을 계산(計算)하는 Element Subroutine 중 3D Beam element, Plate bending element 및 동력학계산(動力學計算)을 위한 Eigenvalue routine을 포함(包含)한 Symbolic Manipulation Program 개발(開發)이다. 이 프로그램의 구조(構造)는 module화(化)된 독립적(獨立的) 기능(機能)을 가진 processor 들로 구성(構成)되어 프로그램의 수정(修正), 첨가(添加), 삭제(削除)가 용이(容易)하며, Integrated Program Network(IPN) 개념중(槪念中) data base 방법(方法)으로 matrix form으로 된 data의 취급이 효율적(效率的)이다.

• 대한토목학회논문집
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• 제30권2A호
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• pp.81-92
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• 2010

강프레임 부재의 설계에서 탄성 시스템좌굴해석은 프레임의 실제 거동을 예측하기 어려운 반면, 비탄성 시스템좌굴해석은 압축부재의 세장비에 따른 비탄성 거동이 고려됨으로써 보다 현실적인 부재의 좌굴거동을 예측할 수 있다. 그러나 시스템좌굴해석 수행후 오일러좌굴식을 이용한 방법은 압축력이 비교적 작게 발생하는 부재에서 과도한 유효좌굴길이를 산정한다는 문제점을 내포하고 있다. 본 연구에서는 강프레임 구조의 모든 부재의 탄성 및 비탄성 유효좌굴길이계수를 산정할 수 있는 새로운 해석방법을 제안하였다. 제안된 방법은 가상축력계수 개념을 기반으로 비탄성 강도감소계수를 도입하고 반복고유치해석을 수행하여 각 부재의 유효좌굴길이계수를 산정한다. 제안된 방법의 타당성을 검증하기 위하여 예제 강프레임 구조물을 제안된 방법에 의거한 유효좌굴길이와 기존 방법에 의거한 결과를 비교하였다. 검증 결과, 제안된 방법은 강프레임의 모든 부재의 탄성 및 비탄성 유효좌굴길이계수를 합리적으로 산정할 수 있었다. 부가적으로 재료의 비탄성 거동이 부재의 유효좌굴길이에 미치는 영향도 논의되었다.