• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2013년도 춘계학술대회 논문집
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• pp.340-346
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• 2013

This paper describes a helicopter vibration induced by main rotor in forward flight. The hub loads in the fixed frame, which are dominant source of helicopter vibration, are obtained by multi-blade summation of rotating blades loadings. The components of 3/rev, 4/rev, and 5/rev blades loadings are transmitted by blades to 4/rev hub loads in the fixed frame. The vertical vibrations of helicopter at pilot seat and copilot seat are calculated through rigid body transfer functions considering airframe to be rigid body. The blades are assumed to be elastic and undergo the flap, lag, and torsion motion and free wake aerodynamic model is used to calculate the precise blade loadings in the analysis. The 4/rev vertical vibration responses are analyzed from rotating blade loadings and fixed hub loadings.

• 대한조선학회지
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• 제25권4호
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• pp.47-57
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• 1988

A new discrete method using idealized rigid body-spring model is introduced. This rigid element method is known to be more efficient and accurate than the finite element method in the inelastic range of structural analysis owing to simplified stress-strain and strain-displacement relations This kind of physical concept using idealized rigid model has been already applied among structural engineers to some problems such as rigid-plastic analysis or plastic design considering rigid bodies and plastic hinges. However the most rigorous and systematic research has been recently performed by T. Kawai et al.[1]. In this paper, an attempt is made to analyze the collapse behavior of stiffened plates under lateral loading by some modification and expansion of Kawai's rigid element approach to the collapse of plates without stiffener. Stiffened plates are treated as orthotropic plates which have equivalent bending rigidities. By employing Morley's plate element resubdivision technique, variety is given to mesh-division styles which have greate effect on the accuracy of numerical results. Some examples are shown to verify the validity of applying rigid element method to the ultimate strength analysis of stiffened plates. It is clarified that lateral deflections and detailed collapse patterns up to the ultimate state of stiffened plates can be easily obtained by the present approach.

• 한국정밀공학회지
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• 제22권4호
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• pp.107-112
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• 2005

In this study, the dynamic analysis is performed fur predicting the transmitted force to flexible human body induced by prototype HIF(High Impulsive force) device operation, which is partially assembled by major parts. A beam-mass model and a shear-structure model are used for the flexible mount structure and their dynamic behavior are investigated by experimental results under rigid/flexible mount conditions using a general purpose device. From the test result of prototype device in rigid mount condition, the transmitted force to human body which can not be measured directly, is estimated based on the proved mount structure model.

• 한국정밀공학회지
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• 제15권7호
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• pp.91-97
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• 1998

The analysis model is the infinite body consisted of power law creep material containing a rigid inclusion with line crack shape subjected to the arbitrarily directional stress on an infinite boundary. The crack analysis is performed using the complex pseudo-stress function. The strain rate intensity factor is determined in the closed form as new fracture mechanics parmeter which represents the magnitudes of stress and strain rate near the tip in power law creep material.

• 대한인간공학회지
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• 제18권3호
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• pp.141-152
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• 1999

In this paper, We performed the human body dynamic modelling for the realistic animation based on the dynamical behavior of human body, and designed controller for the effective control of complicate human dynamic model. The human body was simplified as a rigid body which consists of 18 actuated degrees of freedom for the real time computation. Complex human kinematic mechanism was regarded as a composition of 6 serial kinematic chains : left arm, right arm, support leg, free leg, body, and head. Based on the this kinematic analysis, dynamic model of human body was determined using Newton-Euler formulation recursively. The balance controller was designed in order to control the nonlinear dynamics model of human body. The effectiveness of designed controller was examined by the graphical simulation of human walking motion. The simulation results were compared with the model base control results. And it was demonstrated that, the balance controller showed better performance in mimicking the dynamic motion of human walking.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2004년도 추계학술대회논문집
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• pp.967-971
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• 2004

Today, as the demands for home appliances are increasing, the understanding of noise and vibration characteristics have become more important. It is hard to control its vibration and noise characteristics, because its mechanical structure is very complex. In this study a model of reciprocating compressor is developed. Spring, frame, and LDT are modeled as flexible body, and the other parts are modeled as rigid. FEM model of frame is simplified in order to save the simulation time. We validated the simple model by comparing their natural frequencies and mode shapes. Motor torque is applied to a rotor, and the piston is subjected to a gas pressure. The vibrational characteristics of compressor is analyzed with LS-DYNA. Its results are compared with the simulation results of rigid body frame. The effect of LDT is also studied by comparing the vibration of frame with the results of simulation with no LDT.

• Journal of Advanced Research in Ocean Engineering
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• 제4권4호
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• pp.146-162
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• 2018

The unsteady problem of a rigid body impact onto a floating plate is studied. Both the plate and the water are at rest before impact. The plate motion is caused by the impact force transmitted to the plate through an elastic layer with viscous damping on the top of the plate. The hydrodynamic force is calculated by using the second-order model of plate impact by Iafrati and Korobkin (2011). The present study is concerned with the deceleration experienced by a rigid body during its collision with a floating object. The problem is studied also by a fully-nonlinear computational-fluid-dynamics method. The elastic layer is treated with a moving body-fitted grid, the impacting body with an immersed boundary method, and a discrete-element method is used for the contact-force model. The presence of the elastic layer between the impacting bod- ies may lead to multiple bouncing of them, if the bodies are relatively light, before their interaction is settled and they continue to penetrate together into the water. The present study is motivated by ship slamming in icy waters, and by the effect of ice conditions on conventional free-fall lifeboats.

• 한국컴퓨터그래픽스학회논문지
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• 제27권3호
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• pp.13-23
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• 2021

본 논문에서는 단일 강체 모델(single rigid body)의 무게 중심(center of mass) 좌표계와 발의 위치를 활용하여 캐릭터의 동작을 생성하는 프레임워크를 제안한다. 이 프레임워크를 사용하면 기존의 전신 동작(full body)에 대한 정보를 사용할 때 보다 입력 상태 벡터(input state)의 차원을 줄임으로써 강화 학습의 속도를 개선할 수 있다. 또한 기존의 방법보다 학습 속도를 약 2 시간(약 68% 감소) 감소시켰음에도 기존의 방법 대비 최대 7.5배(약 1500 N)의 외력을 더 견딜 수 있는 더욱 견고한(robust) 모션을 생성할 수 있다. 본 논문에서는 이를 위해 무게 중심의 다음 좌표계를 구하기 위해 중심 역학(centroidal dynamics)을 활용하였고, 이에 필요한 매개 변수(parameter)들과 다음 발의 위치와 접촉력 계산에 필요한 매개 변수들을 구하는 정책(policy)의 학습을 심층 강화 학습(deep reinforcement learning)을 사용하여 구현하였다.

• 전자공학회논문지SC
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• 제37권1호
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• pp.19-29
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• 2000

기존의 위성제어용 시뮬레이션 툴은 위성 모델을 강체로 보고, 비례-미분(Proportional-Differential)제어기를 사용하기 때문에, 이동하는 위성의 경우 오차한계범위를 벗어나 통신이 두절되는 현상이 발생할 수 있다. 따라서, 본 논문은 신속한 자세회복 및 안정된 진보적인 제어기의 설계를 위하여 이동하는 정지궤도 및 저궤도 위성에 대하여 위성을 강체 및 유연체 구조로 모델링하고, 통신두절시 신속한 자세 회복을 위한 최소시간 제어기 설계와 위성의 위치 제어시 발생하는 통신중단을 최소화 하기 위하여 기존의 PD제어기보다 정확하고 안정된 선형조절기를 상태공간 벡터를 사용하여 설계하였다. 시뮬레이션은 먼저 강체 모델과 유연체 모델을 비교하기 위하여, 이동하는 정지궤도 및 저궤도 위성에 대하여 PD제어기를 사용하여 시험되었으며, 자세이동시의 제어기의 응답특성을 분석하기 위하여, 지상의 명령에 의한 위성의 피치각을 변경하는 경우, 주기적으로 수행되는 남북 궤도 유지에 대하여 수행하였다. 그 결과, 강체모델에 대비하여 유연성 모델이 실제 상황에 근접한 결과를 가져다 주었으며, 최소시간제어기는 PD제어기 대비 약 7배 이상 빠르게 신속한 자세 회복을 가져다 주었으며, 선형조절기는 외란에 대한 적응 및 안정도, 응답속도 측면에서 장점을 나타내었다. 향후 이 위성 모델 및 제어기를 사용하여 실제 운용시 예상되는 제어기의 결과를 확인할 수 있으며, 더 나아가 새로운 제어기의 개발 및 교육 등에 유용하게 사용될 수 있을 것이다.

• Ocean and Polar Research
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• 제26권2호
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• pp.323-332
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• 2004

This paper concerns about a study on dynamic responses of tracked vehicle on soft cohesive soil. For dynamic analyses of tracked vehicle, two different models were adopted, i.e. a single-body model and a multi-body model. The single-body vehicle model was assumed as a rigid body with 6-dof. The multi-body vehicle was modeled by using a commercial software, RecurDyn-LM. For the both models properties of cohesive soft soil were modeled by means of three relationships: pressure to sinkage, shear displacement to shear stress, and shear displacement to dynamic sinkage. Traveling performances of the two tracked vehicle models were compared through dynamic analyses in time domain.