• 대한조선학회논문집
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• 제28권1호
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• pp.117-124
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• 1991

본 논문에서는 편면 보강판의 압축 강도 해석 시, 유한 요소법의 비경제성을 극복하기 위하여, 붕괴 양식을 가정하고, 각 붕괴 양식에 대해 압축 강도를 구하였다. 최종 강도는 탄성 대변형 해석 곡선과 소성 붕괴를 가정하여 얻은 소성 해석 곡선과의 교점으로 택하였다. 기존의 연구와는 달리 소성 붕괴선의 형상을 변경시켜 최소의 강도 값을 주는 교점을 최종 강도로 택하였다. 최소 강비는 가정한 붕괴 양식의 교점으로 부터 얻어질 수 있다. 탄성 해석에서는 좌굴 파형을 가정하고, 보강재의 비대칭으로 인한 편심 모우멘트를 고려하였으며, 평형 조건식은 Rayleigh-Ritz법을 이용하여 유도하였다. 소성 해석 시에는 고성 붕괴선을 가정하여 소성 붕괴 조건식을 유도하였다. 좌굴과 최종 강도 계산 결과를 유한 요소법에 의한 결과와 비교한 결과, 양호한 일치를 보였다.

• 한국전자파학회지:전자파기술
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• 제6권4호
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• pp.11-19
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• 1995

본 논문에서는 시간영역 유한차분법(Finite Difference Time Domain : FDTD) 에 의해서 동축선로의 전달계수와 차폐효과에 대하여 해석하고 그 결과를 모멘트법과 비교하였다. 기존의 여기방법인 TE 나 TM 모드를 대신하여 반사파의 빠른 시간내의 완전흡수를 위하여 TEM 모드로 가정한 Gaussian 펄스를 인가하는 방법을 사용하였다. 또한, 동축선로의 차폐효과를 FDTD를 이용하여 계산 결과와 모멘트법을 이요하여 얻은 결괄와 매우 유사한 결과를 얻었다.

• 대한기계학회논문집
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• 제13권4호
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• pp.799-806
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• 1989

본 논문에서는 일반적으로 축방향 변위에 대한 모우드만을 가지고 있는 경우의 합성을 위해 축방향 변위 모우드의 커브-피팅을 이용하여 기울기 정보를 얻고 모델링된 요소의 연결부에 부여함으로써, 변위 정보만을 사용하는 방법보다 좀 더 정확한 고유값을 얻을 수 있음을 보이고자 한다.

• International Journal of Aeronautical and Space Sciences
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• 제18권3호
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• pp.450-466
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• 2017

This paper defines the modified effective membrane stiffness, bending stiffness considering the directionally dependent mechanical properties and mode shape function of a composite lattice rectangular plate, which is assumed to be a Kirchhoff-Love plate. It subsequently presents an approximate method of conducting a buckling analysis of the composite lattice rectangular plate with various boundary conditions under uniform compression using the Ritz method. This method considers the coupled buckling mode as well as the global and local buckling modes. The validity of the present method is verified by comparing the results of the finite element analysis. In addition, this paper performs a parametric analysis to investigate the effects of the design parameters on the critical load and buckling mode shape of the composite lattice rectangular plate based on the present method. The results allow a database to be obtained on the buckling characteristics of composite lattice rectangular plates. Consequently, it is concluded that the present method which facilitates the calculation of the critical load and buckling mode shape according to the design parameters as well as the parametric analysis are very useful not only because of their structural design but also because of the buckling analysis of composite lattice structures.

• 한국통신학회논문지
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• 제19권1호
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• pp.183-193
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• 1994

본 논문에서는 가정모드(assumed mode) 방법과 Lagrange 방식을 이용하여 유연성 로봇 매니퓰레이터의 동력학 방정식을 구하였으며, 조인트 구동기를 포함한 유연성 로봇 매니플레이터에 대한 제어기를 설계를 하였다. 제어기는 매개변수 추정부와 적응제어기로 구성하였으며, 매개변수 추정부는 RLS알고리즘을 이용하여 ARMA예측모델의 매개변수를 추정하도록 하였다. 적응제어기는 기준모델(reference)과 최소예측오차제어기(minimum prediction controller)로 구성하였다.

• Smart Structures and Systems
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• 제25권6호
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• pp.669-678
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• 2020

This paper focuses on the free vibration analysis of axially functionally graded (FG) Euler-Bernoulli beams. The material properties of the beams are assumed to obey the linear law distribution. The complexities in solving differential equation of transverse vibration of composite beams which limit the analytical solution to some special cases are overcome using the Differential Transformation Method (DTM). Natural frequencies and corresponding normalized mode shapes are calculated. Validation targets are experimental data or finite element results. Different parameters such as reinforcement distribution, ratio of the reinforcement Young's modulus to the matrix Young's modulus and ratio of the reinforcement density to the matrix density are taken into investigation. The delivered results prove the capability and the robustness of the applied method. The studied parameters are demonstrated to be very crucial for the normalized natural frequencies and mode shapes.

• 한국소음진동공학회논문집
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• 제18권1호
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• pp.123-130
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• 2008

An analytical method for the free vibration of a flexible rectangular plate in contact with water is developed by the Rayleigh-Ritz method. The plate clamped along the edges is partially contacted with water at both sides. It is assumed that the contained water is incompressible and inviscid. The wet mode shape of the plate is assumed as a combination of the dry mode shapes of a clamped beam. The liquid motion is described by using the liquid displacement potential and determined by using the compatibility conditions along the liquid interface with the plate. Minimizing the Rayleigh quotient based on the energy conservation gives an eigenvalue problem. It is found that the theoretical results can predict excellently the fluid-coupled natural frequencies comparing with the finite element analysis result.

• 한국정밀공학회지
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• 제14권11호
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• pp.34-41
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• 1997

This paper presents a technique to control a very flexible robot moving in a vertical plane. The flexible robot is modeled as an Euler-Bernoulli beam. Elastic deformation is approximated using the assmed modes method. A comparison function which satisfies all geometric and natural boundary conditions of a cantilever beam with an end mass is used as an assumed mode shape. Lagrange's equation is utilized for the development of a discretized model. A control algorithm is developed using a simple PID cnotrol tech- nique. The proportional, integral and deivative control gains are determined based on the dominant pole placement method and tuned to show no overshoot and no steady state error, and short settling time. The effectiveness of the developed control scheme is showed in the hub angular diaplacement control experiment. Three different end masses are uned in the experiment. The experimental results show that developed control algorithm is very effective showing little overshoot, no steady state error, and less than 2.5 second settl- ing time in case of having an end mass which is equivalent to 45% of the manipulator mass. Also the experimental results show that the residual vibration fo the end point is effectively controlled.

• Journal of Mechanical Science and Technology
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• 제20권8호
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• pp.1224-1231
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• 2006

The stability and control derivatives of DURUMI-lI UAV using the flight test are obtained. The flight test data is gathered from the normal flight condition (normal mode) and the flight condition assumed as the right elevator fixed (fault mode). Using real-time parameter estimation techniques, applied to Fourier transform regression method, simulates the aircraft motion. From the result, the fault of control surface is to be detected. In this paper, the results of the real- time parameter estimation techniques are compared with the results of the Advanced Aircraft Analysis (AAA). Using the aerodynamic derivatives, it provides the base line of normal/failure for the control surface by using the on-line parameter estimation of Fourier transform regression. In flight, this approach maybe helpful to detect and isolate the fault of primary control surface. It is explained how to perform the flight condition assumed as the right elevator fixed in the flight test. Also, it is mentioned how to switch between the normal flight condition and the assumed fault flight condition.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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• pp.547-551
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• 1996

In this paper, robust vibration control of a one-link flexible robot arm based on variable structure system is discussed. We derive dynamic equations of it using a Lagrangian assumed modes method based on Bernoulli-Euler Beam theory. The optimal sliding surface is designed and the problem of chattering is also solved by the adoption of a continuous control law within a small neighborhood of the switching hyperplane.