• 제목/요약/키워드: Frequency Response Function Synthesis

검색결과 36건 처리시간 0.023초

혼합모델링을 위한 유한요소모델의 자유도 축소와 보상 (Model reduction and compensation of FE model for Hybrid modelling)

  • 이창호;이시복;이인갑
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 1998년도 춘계학술대회논문집; 용평리조트 타워콘도, 21-22 May 1998
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    • pp.419-425
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    • 1998
  • This paper presents a method of enhancing the accuracy of hybrid modelling that predicts dynamic characteristics of the coupled structure by synthesizing after FE analysis and vibration experimental analysis of the relevant individual substructure. Since most FE models in engineering problems are very large, dynamic analysis with the full FE model is costly. Frequency response function(FRF) synthesis after reducing the FE model can reduce this computational cost but introduce mode truncation error similarly in the case of considering only low-frequency mode after eigensolutions of the complete structure. This paper introduces a FRF of FE model for hybrid FRF synthesis, which is reduced by using IIRS methods and compensated through eigensolutions of the reduced model, and shows the effectiveness of the presented method.

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광디스크 트랙킹 계의 동특성 해석 및 진동 안정화 (Vibration Stabilization of the Tracking System of an Optical Disc Drive)

  • 단병주;최용제
    • 한국정밀공학회지
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    • 제16권1호통권94호
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    • pp.191-199
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    • 1999
  • In designing the tracking system of an optical disc drive, it is first necessary to eliminate the undesired influence of any visible mechanical vibrations. In this paper a geometrical method to analyze the frequency response of an elastically supported planar rigid body has been presented. Using the theory of screw, a geometrical expression of a compliant transfer function which describes the effects of the locations of an applied force and observation on the response has been derived. Applying the substructure synthesis method, a technique to stabilize the tracking mechanical system has been presented with a numerical example.

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부분구조 합성법을 이용한 배기계의 진동해석 (Vibration Analysis of an Exhaust System with Bellows Using the Component Mode Synthesis)

  • 임재문;김민수;이귀영
    • 대한기계학회논문집
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    • 제17권7호
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    • pp.1833-1840
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    • 1993
  • An efficient vibration analysis method, Component Mode Synthesis(CMS), for an exhaust system with bellows is presented. Analyses are performed for two types of bellows, where characteristics of vibration modes affecting idle shake and interior noise of a vehicle are examined. Also analyzed are the contributions of an exhaust and engine mounting system to the idle shake and interios noise. Comparison between the analysis and test is in good agreement, hence the CMS method is shown to be efficient and valid.

프레임 차량의 주행진동 저감을 위한 프레임 부시 복소 동강성 결정에 관한 연구 (A Study on Determination of Complex Stiffness of Frame Bush for Ride-Vibration Improvement of Body-on-Frame Vehicle)

  • 정면규;김기선;김광준;황인진
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2005년도 추계 학술대회논문집(수송기계편)
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    • pp.194-199
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    • 2005
  • Body-on-frame type vehicle has a set of frame bushes which are installed between body and frame fur vibration Isolation. Such frame bushes are important vibration transmission paths to passenger space. In order to reduce the vibration level of passenger space, therefore, the change of complex stiffness of the frame bushes is more efficient than modification of other parts of the vehicle such as body, frame and suspension. The purpose of this study is to reduce the vibration level for ride comfort by optimization of complex stiffness of frame bushes. In order to do this end, simple finite element vehicle model was constructed and the complex stiffness of frame bushes was set to be design variable. Objective function was defined to reflect passenger ride comfort and genetic algorithm and sub-structure synthesis were applied for minimization of the objective function.

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부분구조 모드합성법에 의한 주파수응답함수 산출법 (Calculating Method of FRF with Sub-structure Mode Synthesis Method)

  • 오창근;박경일;박석주
    • Journal of Advanced Marine Engineering and Technology
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    • 제39권4호
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    • pp.393-398
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    • 2015
  • 진동해석에 있어서 매우 중요한 부분 중의 하나가 주파수응답함수를 구하는 것이다. 크거나 복잡한 구조물은 일반적으로 아주 큰 자유도-예를 들면 수 백 만 자유도-를 가지기 때문에 역행렬에 의한 전통적인 방법으로는 주파수응답함수를 구할 수 없을지도 모른다. 그래서 전체 구조물을 몇 개의 부분구조로 나누어서 해석하는 부분구조 해석법을 이용한다. 여기에서는 부분구조별로 나누어 계산한 부분구조 진동모드를 이용하여 자유도를 현격하게 낮춘 등가의 저 자유도 모델에서 주파수응답함수를 구하는 방법을 제시한다. 개발한 프로그램의 신뢰도를 확인하기 위하여 평판 구조물에 적용하여서 실험과 축소하지 않는 영역에서의 해석 결과와 본 해석 결과를 비교하였고, 매우 좋은 결과를 얻었다.

동특성 변경을 위한 구조물의 결합 위치 선정 (Selection of Connection Position to Change Dynamic Characteristic of Structure)

  • 김경원;박윤식;김성훈;김진희;이주훈;황도순
    • 한국소음진동공학회논문집
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    • 제13권12호
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    • pp.930-937
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    • 2003
  • This research deals with how to select connection positions of two substructures to be synthesized. The goal of this research is to find optimal connection positions in order to maximize the fundamental natural frequency of the synthesized structure. The natural frequencies of a connected structure are obtained by modal-force equations. Optimal connection positions can be selected through optimization process. In the optimization process, the natural frequencies of a connected structure are set to object function value and connection positions become design variables. The method described above is applied to synthesis problems of plates, which is initially conducted for FE models and verified through experiments. Especially in experiments. FRF(frequency response function) s are obtained by means of the Modal Testing technique to be used in modal-force equations for synthesizing. Once the substructures are synthesized. the Modal Testing technique is again applied to spot-welded structure using the result from the optimization procedure. It is found that the fundamental natural frequency of the synthesized structure with the optimized result gives higher value than those with the initially given connection positions.

동특성 변경을 위한 구조물의 결합 위치 선정 (Selection of Connection Position to Change Dynamic Characteristic of Structure)

  • 김경원;박윤식;박영진
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2003년도 춘계학술대회논문집
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    • pp.65-71
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    • 2003
  • This research deals with how to select connection positions of two substructures to be synthesized. The goal of this research is to find optimal connection positions in order to maximize the fundamental natural frequency of the synthesized structure. The natural frequencies of a connected structure are obtained by modal-force equations. Optimal connection positions can be selected through optimization process. In the optimization process, the natural frequencies of a connected structure are set to object function value and connection positions become design variables. The method described above is applied to synthesis problems of plates, which is initially conducted for FE models and verified through experiments. Especially in experiments, FRE(frequency Response function)s are obtained by means of the Modal Testing technique to be used in modal-force equations for synthesizing. Once the substructures are synthesized, the Modal Testing technique is again applied to spot-welded structure using the result from the optimization procedure. It is found that the fundamental natural frequency of the synthesized structure with the optimized result gives higher value than those with the initially given connection positions.

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프레임 차량의 주행 진동 저감을 위한 프레임 부시 복소동강성계수 크기 결정에 관한 연구 (A Study on Determination of Complex Stiffness of Frame Bush for Ride-comfort Improvement of Body-on-frame Vehicle)

  • 정면규;김기선;김광준
    • 한국소음진동공학회논문집
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    • 제16권6호
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    • pp.619-626
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    • 2006
  • Body-on-frame type vehicle has a set of frame bushes between body and frame for vibration isolation. Such frame bushes are important vibration transmission paths to passenger space for excitations during driving. In order to reduce the vibration level of passenger space, therefore, change of complex stiffness of the frame bushes is more efficient than modification of other parts of the vehicle such as body, frame and suspension. The purpose of this study is to reduce the vibration level for ride comfort by optimization of complex stiffness of frame bushes. In order to do this, a simple finite element vehicle model was constructed and complex stiffness of the frame bushes was set to be design variables. The objective function was defined to reflect frequency dependence of passenger ride comfort. Genetic algorithm and sub-structure synthesis were applied for minimization of the objective function. After optimization level at a position of interest on the car body was reduced by about 43.7 % in RMS value. Causes for optimization results are discussed.

항공기 시뮬레이터 조종력 제어시스템의 견실 $\mu$-제어기 설계 (Robust $\mu$-Controller design for Control Loading System of Flight Simulator)

  • 방경호
    • 대한전자공학회:학술대회논문집
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    • 대한전자공학회 1998년도 추계종합학술대회 논문집
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    • pp.405-408
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    • 1998
  • Generally, the principle function of simulator control loading system is to provide the pilot or student with the "feel" of the actual aircraft flight control systems during flight, taxing, and in malfunction. Flight control "feel" is the resistance felt by the pilot when moving a control stick or pedal, coupled with the amount of control surface deflection, and hence aircraft response, resulting from the input. Therefore, the control loading servo must be capable of performing to some general list of requirements derived from real aircraft control forces. In this paper, we deal with a $\mu-controller$ design for a control loading system of the flight simulator. For this, we derive a frequency response of the hydraulic system from the identification data and then design a controller using a $\mu-synthesis$ method. Under the same condition of simulation, $\mu-controller$ provides the superior performance than PID controller.than PID controller.

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평판에서 빔 보강재의 결합 위치를 이용한 구조물 변경법 (Structural Dynamics Modification Using Position of Beam Stiffener on Plate)

  • 정의일;박윤식
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 추계학술대회논문집
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    • pp.599-604
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    • 2002
  • Substructures position is considered as design parameter to obtain optimal structural changes to raise its dynamic characteristics. In conventional SDM (structural dynamics modification) method, the layout of modifying substructures position is first fixed and at that condition the structural optimization is performed by using the substructures size and/or material property as design parameters. But in this paper as a design variable substructures global translational and rotational position is treated. For effective structural modification the eigenvalue sensitivity with respect to that design parameter is derived based on measured frequency response function. The optimal structural modification is calculated by combining eigenvalue sensitivities and eigenvalue reanalysis technique iteratively. Numerical examples are presented to the case of beam stiffener optimization to raise the natural frequency of plate.

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