• Title/Summary/Keyword: 전산기구조

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Neuro-Control of Seismically Excited Structures using Semi-active MR Fluid Damper (반능동 MR 유체 감쇠기를 이용한 지진하중을 받는 구조물의 신경망제어)

  • 이헌재;정형조;오주원;이인원
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2002.10a
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    • pp.313-320
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    • 2002
  • A new semi-active control strategy for seismic response reduction using a neuro-controller and a magnetorheological (MR) fluid damper is proposed. The proposed control system consists of the improved neuro-controller and the bang-bang-type controller. The improved neuro-controller, which was developed by employing the training algorithm based on a cost function and the sensitivity evaluation algorithm replacing an emulator neural network, produces the desired active control force, and then the bang-bang-type controller causes the MR fluid damper to generate the desired control force, so long as this force is dissipative. In numerical simulation, a three-story building structure is semi-actively controlled by the trained neural network under the historical earthquake records. The simulation results show that the proposed semi-active neuro-control algorithm is quite effective to reduce seismic responses. In addition, the semi-active control system using MR fluid dampers has many attractive features, such as the bounded-input, bounded-output stability and small energy requirements. The results of this investigation, therefore, indicate that the proposed semi-active neuro-control strategy using MR fluid dampers could be effectively used for control of seismically excited structures.

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Development of Integrated Environment for Optimum Design Using Motif (모티프를 이용한 최적설계 통합환경 개발)

  • Lim, O-Kang;Cho, Heon;Kim,Young-Hyun;Lee, Byung-Woo
    • Computational Structural Engineering
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    • v.9 no.3
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    • pp.97-105
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    • 1996
  • An integrated environment for optimum design has been developed using Motif. The integrated environment is composed of the preprocessor, the postprocessor and the optimization part. The preprocessor is part of making a finite element model for optimum structural design and the postprocessor displays results of optimum design and the optimization part is the part which execute optimization. It is designed to reduce user's difficulties in structural optimum design. It used Graphic User Interface for the concurrent representation of various inputs and outputs through the dialog box, mouse and keyboard. Structural optimum design can be done easily through dialog box, menu, concurrent representation of modeling process and results of structural optimum design can be understood easily through stress contour, deformed model and graph of cost function.

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Nonlinear Response Structural Optimization of a Joined-Wing Using Equivalent Loads (등가하중법을 이용한 접합날개의 기하 비선형 응답 구조최적설계)

  • Kim, Yong-Il;Park, Gyung-Jin
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2007.04a
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    • pp.321-326
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    • 2007
  • The joined-wing is a new concept of the airplane wing. The fore-wing and the aft-wing arc joined together in the joined-wing. The range and loiter are longer than those of a conventional wing. The joined-wing can lead to increased aerodynamic performances and reduction of the structural weight. The structural behavior of the joined-wing has a high geometric nonlinearity according to the external loads. The gust loads are the most critical loading conditions in the structural design of the joined-wing. The nonlinear behavior should be considered in the optimization of the joined-wing. It is well known that conventional nonlinear response optimization is extremely expensive: therefore, the conventional method is almost impossible to use in large scale structures such as the joined-wing. In this research, geometric nonlinear response structural optimization is carried out using equivalent loads. Equivalent loads are the load sets which generate the same response field in linear analysis as that from nonlinear analysis. In the equivalent loads method, the external loads are transformed to the equivalent loads (EL) for linear static analysis, and linear response optimization is carried out based on the EL.

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Numerical Simulation and Verification of Morphing Composite Structure with Embedded SMA Wire Actuators (형상기억합금 선이 삽입된 가변 복합재 패널의 해석 및 실험)

  • Kong, Jung-Pyo;Jung, Beom-Seok;Li, Ningxue;Ahn, Sung-Hoon;Cho, Maeng-Hyo
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2010.04a
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    • pp.343-346
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    • 2010
  • 형상기억합금이 삽입된 복합체는 힌지나 추가적 작동기 없이 그 자체로서 지능 구조의 역할을 할 수 있어 많은 분야에서 활발히 연구되고 있다. 본 논문에서는 형상기억합금(Shape Memory Alloy) 선이 삽입된 $\cap$자형 복합재를 제안하고, 형상기억합금과 모재가 정해진 경우의 곡률 변화에 영향을 주는 주요 설계 변수를 복합재의 너비, 두께, 형상기억합금의 편심률을 설계변수로 가정하고 유한요소 해석과 패널 제작 및 실험을 통해 검증한다. 먼저 라고다스(Lagoudas)모델을 형상기억합금의 구성방정식으로 이용한 유한요소해석모델을 구성하여 수치해석을 수행하고, 11 종류의 형상기억합금 선이 삽입된 유리섬유강화복합재(Glass Fiber Reinforced Plastic) 패널을 제작하여 열하중에 따른 곡률변화를 관찰한다. 해석결과와 실험결과의 비교를 통해 해석모델의 타당성을 검증하며, 해석을 통해 각 설계 변수들의 곡률변화에 대한 영향을 파악한다.

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An Equalization Technique of Dual-Feedback Structure in ATSC DTV Receivers (ATSC DTV 수신기를 위한 이중 후방필터 구조의 결정 궤환 등화기)

  • Oh, Young-Ho;Kim, Dae-Jin
    • Journal of Broadcast Engineering
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    • v.10 no.4 s.29
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    • pp.540-547
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    • 2005
  • In the DFE(Decision Feedback Equalizer) for ATSC DTV receivers, there are decision errors in the slicer or. the simplified trellis decoder, and these decided false data comes to the feedback filter to make the error propagation phenomenon. The error propagation degrades the equalizer performance by increasing residual errors as well as slowing down the convergence rate. In this paper we propose a dual-feedback equalization structure. There are two feedback filters. One is the decision feedback filter which uses the simplified trellis decoder output data, the other is non-decision feedback filter which uses the equalizer output data. The additional non-decision feedback filter doesn't introduce the error propagation, so it can compensate the error propagation. The proposed structure accelerates the convergence rate as well as reduces output men-square error(MSE). We analyzed the performance enhancement of DTV receiver using dual-feedback equalization structure.

Computational Analysis of Vortex Structures around Wall-Mounted Bluff Body in Boundary Layer (경계층 내에 위치한 각진 물체 주위의 와류 전산 해석)

  • Lee, Ju-Yong;Kim, Hyeon-U;Lee, Seung-Su
    • Proceeding of EDISON Challenge
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    • 2013.04a
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    • pp.354-359
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    • 2013
  • 일반적으로 건축물의 설계시 풍동 실험을 통한 풍환경의 평가를 수행하고 있으며, 이는 환경 영향 평가법에서 정한 건축 사업 시행 시 수반되어야 할 자연환경, 생활환경 그리고 사회경제환경의 영향 평가의 일환으로 실시되고 있다. 그러나, 풍동 실험의 경우 여러 가지 현실적 제약조건으로 설계와 실험의 피드백 (Feedback)이 원활하지 못하며, 특히 대상 건축물이 공장과 같이 대기 오염원이 되는 경우 실험은 더욱 어려운 형편이다. 이에 대한 보완책으로 전산 유체 역학을 이용한 건축물의 풍압 해석에 의한 풍하중 추정이나 인접 지형-지물의 영향을 고려한 건축물 주위의 풍환경 평가가 있다. 전산 모사에 의해 풍동 실험의 미비점을 보완하고, 보다 상세한 정보를 확보함으로써 건축물의 구조적 안전성의 증대와 환경 피해 감소를 기할 수 있다. 그러나 복잡한 지형-지물이나 건축물 주위의 풍환경에 대한 전산 모사는 주로 두 가지의 기술적 어려움을 수반하게 되다. 그 중 하나는 고정 경계면을 이루는 형상의 복잡성으로 인해 기존에 많이 이용하고 있는 Body-fitted 격자계를 이용하는 경우, 격자 생성 과정이 매우 복잡하고 어려울 뿐 만 아니라 생성된 격자가 주로 비정렬 (unstructured) 특성을 갖게 되어 수치해석 과정의 효율을 저하시키는 요인이 되며, 격자의 형상도 수치해석의 수렴성을 저하시키는 예가 많다. 다른 어려움으로 풍환경은 전형적인 난류 유동장으로서 난류의 전산 해석은 아직도 해결하지 못한 부분이 많다는 점이다. 이에 본 논문에서는 복잡한 지형-지물이나 건축물의 풍하중과 풍환경의 전산 모사 기술 확보를 위하여 수행중인 연구의 일환으로 물체 형상의 기하학적 복잡성의 극복을 위한 가상경계법 (Immersed Boundary Method)과 난류 유동장의 물리적 엄밀성을 높이기 위한 다와동 모사 (Large Eddy Simulation)을 이용한 물체 형상과 무관한 유동장 해석 기술 개발에 대하여 다루고자 한다. 먼저 최근에 유동 해석에 이용되는 방법인 가상경계법(IBM)은 물체를 포함한 전체 전산 영역을 직교 좌표계에 의해 이산화하고, 유동장내 존재하는 물체의 표면에서의 점착 조건을 만족시키기 위하여 지배 방정식에 적절한 외력을 추가로 고려하는 방법이다. 본 연구에서는 가상경계법을 이용하여 경계층에 위치한 건물 형상의 각진 물체 주위 사이에 형성되는 공동 내부의 비정상 유속 및 압력에 대한 전산 해석을 수행하고, 풍상측 전면에 형성되는 경계층에 의한 영향을 분석하였다.

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A Static Fluid-Structure Interaction Analysis System Based on the Navier-Stokes Equations for the Prediction of Aerodynamic Characteristics of Aircraft (항공기 공력특성 예측을 위한 Navier-Stokes 방정식 기반의 정적 유체-구조 연계 해석 시스템)

  • Jung, Sun-Ki;Anh Duong, Hoang;Lee, Young-Min;Lee, Jin-Hee;Myong, Rho-Shin;Cho, Tae-Hwan
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.6
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    • pp.532-540
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    • 2008
  • Recently there are growing interests in calculating aerodynamic characteristics of aircraft configurations with structural deformation using the FSI(Fluid-Structure Interaction) system in which CFD(Computational Fluid Dynamics) and CSD(Computational Structure Dynamics) modules are coupled. In this paper the FSI system comprised of CAD, CFD, CSD, VSI(Volume Spline Interpolation) and grid deformation modules was constructed in order to investigate aerodynamic characteristics of the deformed shape. In the process VSI and grid generation modules are developed to combine CSD and CFD routines and to regenerate the aerodynamic grids for the deformed shape, respectively. For the CFD and CSD analysis, commercial programs FLUENT and NASTRAN were used. As a test model, DLR-F4 wing configuration was chosen and its aerodynamic characteristics were calculated by applying the static FSI system. It was shown that lift and drag coefficients of the wing at mach number 0.75 are reduced to 20.26% and 18.5%, respectively, owing to the structural deformation.

상 분리 메커니즘에 의한 3차원 규칙 배열 다공 구조 형성 시뮬레이션

  • Kim, Dong-Uk;Cha, Pil-Ryeong;Byeon, Ji-Yeong
    • Proceedings of the Materials Research Society of Korea Conference
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    • 2011.05a
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    • pp.241.2-241.2
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    • 2011
  • 다공 소재는 큰 비표면적과 규칙적으로 정렬된 구조의 특성으로 인해 자성메모리 소자용 재료, 나노 와이어 제작용 템플릿, 마이크로 반응기, 메타물질용 소재 등으로 각광을 받고 있다. 자기조립 수직배열 다공구조 재료를 제작하는 방법으로 흔히 알루미늄의 양극산화 방법과 이원공정계의 상분리 방법이 등이 있다. 본 연구에서는 상변태를 비롯한 패턴형성과 계면 운동을 가장 정확하게 다루는 이론적 모델로 알려진 상장모델(Phase Field model)을 이용하여 이원공정계의 박막성장과정 동안의 자발적 상분리에 의한 수직배열 자기조립 다공구조 형성을 시뮬레이션 한다. 상장모델을 기초로 하여 상분리 메커니즘에 의해 발현된 미세조직을 해석하고 다양한 공정변수가 미세조직 발현에 미치는 영향에 대해 연구한다. 또한 상장모델을 통해 얻은 결과는 기존에 발표된 연구들의 결과와 비교를 통해 유효성을 입증한다.

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Inter-story Drift Design Method to Improve the Seismic Performance for Steel Moment Frames (철골모멘트골조의 내진성능향상을 위한 층간변위조절기법)

  • Choi, Se-Woon;Park, Hyo-Seon
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.24 no.6
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    • pp.707-714
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    • 2011
  • The inter-story drift ratio is used to evaluate the damage of buildings by the earthquake. This is known that as the inter-story drift ratio decreases, the seismic damage decreases. Although to reduce the inter-story drift ratio is the important issue in the seismic design, no practical inter-story drift design method has bean developed. This study presents an optimal inter-story drift design method to improve the seismic performance of the steel moment frames using the resizing algorithm. The objective function of the proposed method is to minimize the differences of the inter-story drift ratios so that the inter-story drift ratios of the building could be distributed evenly and be reduced. Because this method redesigns the sectional properties of structural members base on the displacement participation factor calculated by the unit-load method, this can improve the seismic performance of the structure without the iterative structural analysis. The efficiency of this algorithm was demonstrated by the application to steel moment frames.

Optimal Transducer Placement for Health Monitoring of Large Structural System (대형 구조물의 상설 감지를 위한 감지기의 최적 위치)

  • 황충열;허광희
    • Computational Structural Engineering
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    • v.10 no.3
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    • pp.157-165
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    • 1997
  • This research aims to develop an algorithm of optimal transducer placement for health monitoring of large structural system. The structural vibration response-based health monitoring is considered one of the best for the system which requires a long-term, continuous monitoring. In its experimental modal testing, however, it is difficult to decide on the measurement locations and their number, especially for complex structures, which have a major influence on the quality of the results. In order to minimize the number of sensing operations and optimize the transducer location while maximizing the accuracy of results, this paper discusses about an optimum transducer placement criterion suitable for the identification of structural damage for continuous health monitoring. As a criterion algorithm, it proposes the Kinetic Energy Optimization Technique (EOT), and then addresses the numerical issues which are subsequently applicable to actual experiment where a bridge model is used. By using the experimental data, it compares the EOT with the EIM(Effective Indefence Method) which is generally used to optimize the transducer placement for the damage identification and control purposes. The comparison conclusively shows that the EOT algorithm proposed in this paper is preferable when a structure is to be instrumented with fewer sensors for monitoring purpose.

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