• 제목/요약/키워드: External forces

검색결과 739건 처리시간 0.026초

원유 생산.저장.하역선의 갑판침수에 관한 연구 (A Study on the Deck Wetness of the FPSO)

  • 임춘규;이호영
    • 대한조선학회논문집
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    • 제41권1호
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    • pp.8-14
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    • 2004
  • As the number of offshore structure is glowing in deep waters, there have been increased damages of it. These floating structures in offshore locations exposed to harsh environmental conditions. In recent years, there has been a slowing attention around damages on bow and deck on FPSO caused by waves in steep storm condition. This paper describes a study of the water on deck due to the dynamic behavior of a FPSO with turret mooring system. The nonlinear motions of the FPSO are simulated under external forces due to wave, current, wind, and mooring forces in the time domain. The direct integration method is employed to estimate low frequency drift wave forces. The current forces are calculated by using slow motion maneuvering equations in the horizontal plane. The coefficients of a model for wind forces are calculated from Isherwood's experimental data and the variation of wind speed is estimated by wind spectrum according to the guidelines of API-RP2A.

천수역에서 외력하에 근접 항행중인 선박의 안전조선에 관한 연구 (A Study on the Safe Manoeuvring of Ships Navigating in Shallow Water under Strong Environmental Forces)

  • 이춘기
    • 한국항해항만학회지
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    • 제34권10호
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    • pp.735-740
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    • 2010
  • 이 연구는 천수역에서 강한 바람과 조류하에 근접 항행중인 두 선박간의 상호유체력이 선박조종운동에 미치는 영향에 대해서 다룬다. 천수역에서 추월 및 피추월관계에 있는 대형선박의 조종운동은 바람, 조류 및 두 선박간의 상호유체력으로 인하여 상당히 복잡해진다. 이 연구의 목적은 안전항행을 위하여 천수역에서 강한 바람 및 조류하에 근접 항행중인 두 대형선박에게 요구되어지는 두 선박간의 속도에 따른 안전항과거리에 대해서 검토, 고찰하고자 한다.

외력에 반응하는 인간형 로봇의 머리를 위한 6 축 힘/모멘트 센서 개발 (Development of 6-axis Force/moment Sensor for Humanoid Robot's Head Reacting to a External Force)

  • 김갑순
    • 한국정밀공학회지
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    • 제26권12호
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    • pp.78-84
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    • 2009
  • When external force is applied to humanoid robot's head, humanoid robot's neck is rotated to prevent the damage of it. So, robot's neck have to perceive forces (Fx of x-direction, Fy of y-direction and Fz of z-direction) and moments (Mx of x-direction, My of y-direction and Mz of z-direction) using the attached 6-axis force/moment sensor. Thus, in this paper, 6-axis force/moment sensor was developed to sense the forces and moments applied to robot's head. The structure of 6-axis force/moment sensor was modeled newly, and it was designed using FEM software (ANSYS) and manufactured by attaching straingages on the sensing element, finally, the characteristic test of the sensor was carried out. As a result, it is confirmed that interference error is less than 3%. And, it is thought that the sensor can be used to measure the forces and the moments for humanoid robot's head.

통합모델과 최적 경로설계를 통한 산업용 로봇 동적 매개변수 규명 (Optimal Excitation Trajectories for the Dynamic Parameter Identification of Industrial Robots by Using Combined Model)

  • 박경조
    • 동력기계공학회지
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    • 제12권2호
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    • pp.55-61
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    • 2008
  • This paper discusses the advantages of using Fourier-based periodic excitation and of combining internal and external models in dynamic robot parameter identification. Internal models relate the joint torques or forces with the motion of the robot; external models relate the reaction forces and torques on the bedplate with the motion data. This combined model allows to combine joint torque/force and reaction torque/force measurements in one parameter estimation scheme. This combined model estimation will yield more accurate parameter estimates, and consequently better predictions of actuator torque, which is shown by means of a simulated experiment on a CRS A465 industrial robot.

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외력과 부싱변형을 고려한 무질량 링크 모델 개발 (Development of the Massless Link Model including External Force and Bushing Deformation)

  • 손정현;최성태;김광석;유완석;이종년
    • 한국자동차공학회논문집
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    • 제9권1호
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    • pp.163-170
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    • 2001
  • In this paper, a massless link model transmitting external forces is developed to achieve the numerical efficiency in simulation of vehicle suspension systems. Forces acting on links are resolved and transmitted to attached points with a quasi-static assumption. Also, a theoretical derivation and computer implementation of a massless link with bushing elements are proposed. In the massless link with bushing elements, one end is connected to the adjacent body with bushings and the other end is connected with a spherical joint. The deformation of a massless link with bushing elements is theoretically determined by minimizing the potential energy function with quasi-static equilibrium assumption at each time step. Several simulations with a full vehicle model are carried out to compare the efficiency of the developed massless link component. From the results, it is concluded that the proposed approach can reduce the computational time considerably.

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실감성 향상을 위한 변형 물체 모델 (Deformable Object Model for Improving Reality)

  • 전성원;김영일;허진헌;전차수;박세형
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2004년도 추계학술대회 논문집
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    • pp.768-773
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    • 2004
  • Developed in this paper a mass-spring engine to represent and manipulate deformable objects. The deformable object model is a basic technology in the ‘Tangible Space Initiative’. The mass-spring model consists of structural, shear and bending springs. Various forces like external, friction, gravity, spring, and damping forces are considered and collision with planes and spheres are treated. When a sphere collide mass-spring model, mass-spring engine calculates external force to interface mass-spring model. A prototype system is implemented in C on an MS windows machine.

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압전세라믹 외팔보형 진동센서의 설계 및 제작 (Design and Fabrication of Piezoceramic Cantilever Type Vibration Sensors)

  • 정이봉;노용래
    • 소음진동
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    • 제7권3호
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    • pp.377-386
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    • 1997
  • A cantilever type piezoceramic vibration sensor was developed that could make up for the short-comings of current vibration sensors, such as high price, low sensitivity, and complex structure. For the design, in conjunction with piezoelectric constitutive equations, we derived full analytic response equations of the piezoelectric bimorph sensor to external forces. The external forces were supposed to take the form of either step or sinusoidal force. Based on the results, actual piezoelectric vibration sensors were fabricated and tested for verification of the theoretical results. Further, comparison of the performance of the developed sensor was made with that of a commercially available representative vibration sensor so that quantitative evaluation of its sensitivity could be made. The sensor developed in this work showed excellent sensitivity and thermal stability in addition to the merits of simple structure and low fabrication cost in comparison with conventional mass-loaded piezoelectric sensors.

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골조 파이프 구조물의 최적신뢰성 설계 (Reliability-Based Optimum Design for Tubular Frame Structures)

  • 백점기
    • 한국해양공학회지
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    • 제2권1호
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    • pp.95-105
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    • 1988
  • This paper describes the development of a reliability-based optimum design technique for such three dimensional tubular frames as off shore structures. The objective function is formulated for the structural weight. Constraints that probability of failure for the critical sections does not exceed the allowable probability of failure are set up. In the evaluation of the probability of failure, fatigue as well as buckling and plasticity failure are taken into account and the mean-value first-order second-moment method(MVFOSM) is applied for its calculation. In order to reduce the computing time required for the repeated structural analysis in the optimization process, reanalysis method is also applied. Application to two and three dimensional simple frame structures is performed. The influence of material properties, external forces, allowable failure probabilities and interaction between external forces on the optimum design is investigated.

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헬리콥터 탑재 비행 시험을 위한 파드 시스템 구조 설계 (Structural Design of pod system for Helicopter Captive Flight Test)

  • 최장섭
    • 한국군사과학기술학회지
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    • 제16권6호
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    • pp.779-788
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    • 2013
  • The load requirements should be known to design mechanical structure. This paper proposes a generation method of load requirements using U.S. military specification to design the external mounting structure of the helicopters of which the flight environments such as aerodynamic forces and inertia forces are unknown. In this study, the load requirements which were applied at the design of the pod structure for helicopter captive flight test could be computed by using this method. The validation of proposed method was confirmed from the test flight using developed pod system.

임피던스 방식에 의한 로보트 매니퓰레이터의 슬라이딩 모드 제어 (Sliding Mode Control of a Robot Manipulator by the Impedance Approach)

  • 최형식
    • Journal of Advanced Marine Engineering and Technology
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    • 제18권4호
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    • pp.25-32
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    • 1994
  • This paper presents a robust impedance controller design to coordinate a robot manipulator under system uncertainties while regulating external forces. By an impedance approach, the relationship between the motion and external forces is defined. Due to the system uncertainties, two kind of sliding mode control schemes based on the impedance approach are derived to ensure that the manipulator end-effector follows a desired trajectory and the force applied to end effector is regulated according to a target impendance. A stability condition is shown according to a sliding condition. To evaluate the devised control scheme, a numerical example is shown.

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