• 제목/요약/키워드: normal mode method

검색결과 307건 처리시간 0.02초

비선형 정규모드를 이용한 보의 비평면 자유진동해석 (Analysis of Nonplanar Free Vibrations of a Beam by Nonlinear Normal Mode)

  • 이원경;이규수;박철희
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2000년도 춘계학술대회논문집
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    • pp.441-448
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    • 2000
  • An investigation into the nonlinear free vibrations of a cantilever beam which can have not only planar motion but also nonplanar motion is made. Using Galerkin's method based on the first mode in each motion, we transform the boundary and initial value problem into an initial value problem of two-degree-of-freedom system. The system turns out to have two normal modes. By Synge's stability concept we examine the stability of each mode. In order to check validity of the stability we obtain the numerical Poincare map of the motions neighboring on each mode.

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가변 블록 부호화에서 CBP를 이용한 고속 인터모드 결정 방법 (Fast Intermode Decision Method Using CBP on Variable Block Coding)

  • 류권열
    • 한국정보통신학회논문지
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    • 제14권7호
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    • pp.1589-1596
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    • 2010
  • 본 논문에서는 CBP(coded block pattern) 및 colocated-MB(macro block)의 부호화 정보를 이용하여 인터모드 결정에 소요되는 계산량을 감소시키는 방법을 제안한다. 제안한 방법은 MB를 CBP 특성에 따라 best-CBP와 normal-CBP 로 나눈다. Best-CBP에서는 SKIP 모드 및 M-Type 모드일 확률이 통계적으로 96.3%이므로 인터모드 결정 과정에서 $8{\times}8$ 모드 계산을 제거한다. Normal-CBP에서는 SKIP 모드 및 M-Type 모드 결정에 colocated-MB의 부호화 정보와 MVcost(motion vector cost)를 이용하여 비트율-왜곡 치에 소요되는 계산량을 선택적으로 제거한다. 실험 결과, 제안한 방법은 전체 부호화 시간이 평균적으로 58.44% 감소되었으며, 움직임이 적은 영상에서 계산량 감소 효과가 우수함을 알 수 있었다.

Ritz 벡터를 이용한 수정 분할구조해석법 (Modified Component Mode Synthesis Method Using Ritz Vectors)

  • 이인원;김동옥
    • 소음진동
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    • 제3권1호
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    • pp.77-82
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    • 1993
  • In general, the dynamic analysis with FEM(Finite Element Method) of large structures requires large computer memory space and long computational time. For the purpose of economical dynamic analysis of large structures, most of engineers want to use an efficient solution algorithm. This paper reports the modified CMS(Component Mode Synthesis) method which uses more efficient algorithm than the classical CMS method. In this paper, it is shown that Ritz vector sets can play the role of normal mode vector sets of substurctures in the CMS algorithm. The modified CMS method has good convergence performance compared with that of the classical CMS method.

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정규모드의 안정성 변화에 따른 분기모우드의 계산법 (Computations of bifurcating modes due to the stability change of normal modes)

  • 박철희
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2000년도 춘계학술대회논문집
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    • pp.435-440
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    • 2000
  • It is shown, in nonlinear two-degree-of freedom system, that the bifurcating modes are created by the stability changes of normal modes. There are four types of stability criterion, each of which gives rise to a distinct functional form of bifurcating modes; the bifurcating mode is born in the form of eigenfunction through which the stability is changed. Then a procedure is formulated to compute the bifurcating mode by the method of harmonic balance. Application of bifurcating mode to forced vibrations is introduced.

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MIC를 위한 2선 및 3선 결합선로의 Quasi TEM Mode 정수계산

  • 류범;김청식;진년강
    • 한국통신학회:학술대회논문집
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    • 한국통신학회 1986년도 춘계학술발표회 논문집
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    • pp.194-197
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    • 1986
  • The normal mode parameters of microstrip coupled lines are datermined from the self and mutual capacitance and inductance of microstrip lines. In this paper, these capacitance are computed by using the relaxation method based on Quas1-TEM model for shoelded structure. Using these results, the normal mode parameters of two and three microstrip coupled lines are obtained.

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모드해석을 이용한 L, T 자형 구조물의 결합 강성 평가 방법에 대한 연구 (The Study of Stiffness Evaluation Technique for L, T Shaped Joint Structures Using Normal Modes Analysis with Lumped Mass)

  • 허덕재;정재엽;조연;박태원
    • 소음진동
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    • 제9권5호
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    • pp.975-983
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    • 1999
  • This paper describes the dynamic characteristics of the joint structures in case of using the simplified beam model in the F. E. analysis. The modeling errors, when replace the shell with the beam, are investigated through F. E. normal modes analysis. Normal mode analysis were performed to obtain the natural frequencies of the L and T shaped joints with various type of channels. The results were analyzed to access the effects of the models on the accuracy of F.E. analysis by identifying the geometric factors which cause the error. The geometric factors considered are joint angle, channel length, thickness and area ratio of the hollow section to the filled one. The joint stiffness evaluation technique is developed in this study using normal modes analysis with Lumped Mass. With this method, the progressively improved results of F. E. analysis are obtained using the simplified beam model. The static and normal modes analysis are performed with the joint stiffness values obtained by the Kazunori Shimonkakis' virtual stiffness method and the proposed method and these simplified modeling errors are compared.

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비선형 경계조건을 가진 보의 정규모드진동 (Normal Mode Vibrations of a Beam with a Nonlinear Boundary Condition)

  • 김현기;이원경
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 1998년도 춘계학술대회논문집; 용평리조트 타워콘도, 21-22 May 1998
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    • pp.392-398
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    • 1998
  • In order to check the validity of nonlinear normal modes of continuous, systems by means of the energy-based formulation, we consider a beam with a nonlinear boundary condition. The initial and boundary e c6nsl of a linear partial differential equation and a nonlinear boundary condition is reduced to a linear boundary value problem consisting of an 8th order ordinary differential equations and linear boundary conditions. After obtaining the asymptotic solution corresponding to each normal mode, we compare this with numerical results by the finite element method.

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A Study on the Real-Time Parameter Estimation of DURUMI-II for Control Surface Fault Using Flight Test Data (Longitudinal Motion)

  • Park, Wook-Je;Kim, Eung-Tai;Song, Yong-Kyu;Ko, Bong-Jin
    • International Journal of Control, Automation, and Systems
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    • 제5권4호
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    • pp.410-418
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    • 2007
  • For the purpose of fault detection of the primary control surface, real-time estimation of the longitudinal stability and control derivatives of the DURUMI-II using the flight data is considered in this paper. The DURUM-II, a research UAV developed by KARI, is designed to have split control surfaces for the redundancy and to guarantee safety during the fault mode flight test. For fault mode analysis, the right elevator was deliberately fixed to the specified deflection condition. This study also mentions how to implement the multi-step control input efficiently, and how to switch between the normal mode and the fault mode during the flight test. As a realtime parameter estimation technique, Fourier transform regression method was used and the estimated data was compared with the results of the analytical method and the other available method. The aerodynamic derivatives estimated from the normal mode flight data and the fault mode data are compared and the possibility to detect the elevator fault by monitoring the control derivative estimated in real time by the computer onboard was discussed.

연성모드법 기반의 원거리 비상관 해저면 잔향음 모델 (Long range incoherent seafloor reverberation model based on coupled normal mode method)

  • 박중용;추영민;이근화;성우제
    • 한국음향학회지
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    • 제35권4호
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    • pp.243-252
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    • 2016
  • 본 논문에서는 연성 모드 기반의 양상태 비상관 잔향음 모델을 제안한다. 거리종속 환경에서 단방향 연성모드 기반의 음파전달모델을 사용하여 음원에서의 산란체에 도달하는 음압과 산란체에서 수신원에 도달하는 음압을 계산한다. 계산의 편의 상 각 산란체와 음원 또는 수신기 사이의 음파전달은 산란체와 음원 또는 수신기를 잇는 2차원 평면에서만 일어난다고 가정한다. 모델의 타당성을 검증하기 위해, 미 해군 잔향음 모델링 워크숍 I, II에 제시된 문제에 대해 계산하고, 그 결과를 음선 이론 기반의 비상관 잔향음 결과와 비교했다.

유연성을 가진 기계 시스템의 동역학 해석 (DYNAMIC ANALYSIS OF A MECHANICAL SYSTEM WITH FLEXIBLE BODIES)

  • 박태원;서종휘;정원선;채장수;서현석
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집B
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    • pp.422-427
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    • 2001
  • The component mode synthesis method allows the elastic deformation of each component in the flexible multibody system by a sum of modes and modal coordinates. This paper focuses on the selection of boundary conditions and deformation modes for redundantly constrained flexible components in mechanical system dynamics. The result of a flexible body dynamic analysis with only normal modes is used to identify proper boundary conditions of a static modes and a desired set of static modes which will be used in the final model. A simple four bar mechanism is used to explain the procedure and a space satellite with solar panels is analyzed using the proposed method.

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