• 제목/요약/키워드: Newton-Euler

검색결과 59건 처리시간 0.022초

Hysteretic model for stud connection in composite structures

  • Xi Qin;Guotao Yang
    • Steel and Composite Structures
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    • 제47권5호
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    • pp.587-599
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    • 2023
  • The establishment of a hysteretic model which can accurately predict the hysteretic characteristics of the stud connection is of utmost importance for the seismic assessment of composite structures. In this paper, the Bouc-Wen-Baber-Noori(BWBN) model was adopted to describe the typical hysteretic characteristics of stud connections. Meanwhile, the Newton-Raphson iterative procedure and the Backward Euler method were used to determine the restoring force, and the Genetic Algorithm was employed to identify the parameters of the BWBN model based on the experimental data consisting of eight specimens. The accuracy of the identified parameters was demonstrated by comparison with the experimental data. Finally, prediction equations for the BWBN model parameters were developed in terms of the physical parameters of stud connections, which provides an approach to get the hysteretic response of stud connections conveniently.

Estimation algorithms of the model parameters of robotic manipulators

  • Ha, In-Joong;Ko, Myoung-Sam;Kwon, Seok-Ki
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1987년도 한국자동제어학술회의논문집(한일합동학술편); 한국과학기술대학, 충남; 16-17 Oct. 1987
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    • pp.932-938
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    • 1987
  • The dynamic equations of robotic manipulators can be derived from either Newton-Euler equation or Lagrangian equation. Model parameters which appear in the resulting dynamic equation are the nonlinear functions of both the inertial parameters and the geometric parameters of robotic manipulators. The identification of the model parameters is important for advanced robot control. In the previous methods for the identification of the model parameters, the geometric parameters are required to be predetermined, or the robotic manipulators are required to follow some special motions. In this paper, we propose an approach to the identification of the model parameters, in which prior knowledge of the geometric parameters is not necessary. We show that the estimation equation for the model parameters can be formulated in an upper block triangular form. Utilizing the special structures, we obtain a simplified least-square estimation algorithm for the model parameter identification. To illustrate the practical use of our method, a 4DOF SCARA robot is examined.

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상하동요 감쇠장치 적용을 통한 새로운 다물체동역학 프로그램의 적용성 검토 (Study on the Applicability of a New Multi-body Dynamics Program Through the Application to the Heave Compensation System)

  • 구남국;하솔;노명일
    • 한국전산구조공학회논문집
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    • 제26권4호
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    • pp.247-254
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    • 2013
  • 본 논문에서는 해상 시추작업을 위한 heave compensation system의 시뮬레이션 모델을 개발하였다. 우선 시뮬레이션을 위하여, 다물체계 동역학 커널을 개발하였다. 다물체계 동역학 커널은 입력 받은 heave compensation system 시뮬레이션 모델의 운동학적 정보를 이용하여 recursive Newton-Euler formulation 방법을 기반으로 운동방정식을 자동으로 구성하고, 수치적으로 해를 계산하는 기능을 한다. 그리고 해상 시추선에 작용하는 외력을 계산하기 위하여 유체 정역학적 힘과 유체 동역학적 힘을 계산하는 모듈을 개발하였다. 이와 같이 개발한 커널과 모듈들을 적용하여 해상 시추선의 hoisting system 동적거동 해석을 수행하고, 관절에서의 구속력을 계산하였다.

중첩 격자를 이용한 제자리 및 전진 비행하는 헬리콥터 로터의 비정상 공력해석 (Unsteady Aerodynamic Analysis for Helicopter Rotor in Hovering and Forward Flight Using Overlapped Grid)

  • 임동균;위성용;김유진;권장혁;이덕주;박수형;정기훈;김승범
    • 한국항공우주학회지
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    • 제37권3호
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    • pp.215-223
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    • 2009
  • 본 연구에서는 헬리콥터 로터 블레이드의 움직임을 모사하기 위해 중첩 격자 기법을 적용하여 헬리콥터 로터의 전진 및 제자리 비행을 모사하였다. 제자리 및 무양력 전진 비행은 Caradonna & Tung의 로터 블레이드를 적용하였으며 전진 비행은 AH-1G 로터 블레이드를 적용하여 수치해석 하였다. 전진 비행 시 cyclic pitch각에 대해서 Newton-Raphson 수렴 방법으로 수치 트림을 수행하였으며 수치 트림에 의한 결과를 실험 및 다른 수치해석 결과와 비교하였을 때 실험값과 유사한 결과를 얻었다. 또한 수치 트림에 의한 결과는 로터 전진면에서 나타나는 BVI 현상을 잘 모사하였다. 지배 방정식은 3차원 비정상 오일러 방정식을 사용하였으며 원방 경계 조건으로 리만 불변치 경계조건을 적용하였다.

MRAC 기법을 이용한 무인 컨테이너 운송차량의 조향 제어 (Steering Control of Unmaned Container Transporter Using MRAC)

  • 이영진;허남;최재영;이권순;이만형
    • 한국항만학회지
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    • 제14권3호
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    • pp.291-301
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    • 2000
  • T his paper presents the lateral and longitudinal control algorithm for the driving of a 4WS AGV(Automated Guided Vehicle). The control law to the lateral and longitudinal control of the AGV includes adaptive agin tuning ability, that is the controller gain of the gravity compensated PD controller can be changed on a real-time. The gain tuning law is derived from the Lyapunov direct method using the output error of the reference model and the actual model, And to show the performance of the presented lateral and longitudinal control algorithm, we simulate toe nonlinear AGV equations of the motion by deriving the Newton-Euler Method, The read path is from quay yard area to docking position in loading yard area. The quay yard area is where the quay crane loads the container to the AGV and the docking position is where the container is transferred to the gantry crane. The road types are constructed in a straight line and J-turn. When driving the straight line, the driving velocity is 6㎧ and the J-turn is 3㎧.

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Post-buckling analysis of aorta artery under axial compression loads

  • Akbas, Seref Doguscan;Mercan, Kadir;Civalek, Omer
    • Advances in nano research
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    • 제8권3호
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    • pp.255-264
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    • 2020
  • Buckling and post-buckling cases are often occurred in aorta artery because it affected by higher pressure. Also, its stability has a vital importance to humans and animals. The loss of stability in arteries may lead to arterial tortuosity and kinking. In this paper, post-buckling analysis of aorta artery is investigated under axial compression loads on the basis of Euler-Bernoulli beam theory by using finite element method. It is known that post-buckling problems are geometrically nonlinear problems. In the geometrically nonlinear model, the Von Karman nonlinear kinematic relationship is employed. Two types of support conditions for the aorta artery are considered. The considered non-linear problem is solved by using incremental displacement-based finite element method in conjunction with Newton-Raphson iteration method. The aorta artery is modeled as a cylindrical tube with different average diameters. In the numerical results, the effects of the geometry parameters of aorta artery on the post-buckling case are investigated in detail. Nonlinear deflections and critical buckling loads are obtained and discussed on the post-buckling case.

이족 보행 로보트를 위한 3차원 모의 실험기의 개발 (Development of 3D simulator for biped robot)

  • 김민수;이보희;김진걸
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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    • pp.928-931
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    • 1996
  • It is necessary to develop the simulator for the test of stability and torque before the walking experiment of biped robot, because a robot may be damaged in an actual experiment. This thesis deals with the development of three-dimensional simulator for improving efficiency and safety during development and experimentation. The simulator is composed of three parts-solving dynamics, rendering pictures and communicating with the robot. In the first part, the D-H parameter and parameter of links can be loaded from the file and edited in the program. The results are obtained by using the Newton-Euler method and are stored in the file. Through the above process, the proper length of link and driving force can be found by using simulator before designing the robot. The second part is organized so that the user can easily see a specific value or a portion he wants by setting viewing parameters interactively. A robot is also shown as a shaded rendering picture in this part. In the last part, the simulator sends each desired angle of joints to the robot controller and each real angle of joints is taken from the controller and passed to the second part. The safety of the experiment is improved by driving the robot after checking whether the robot can be actuatable or not and whether the ZMP is located within the sole of the foot or not for a specific gait. The state of the robot can be easily grasped by showing the shaded rendering picture which displays the position of the ZMP, the driving force and the shape of robot.

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Development of Inverse Dynamic Controller for Industrial robots with HyRoHILS system

  • Yeon, Je-Sung;Kim, Eui-Jin;Lee, Sang-Hun;Park, Jong-Hyeon;Hur, Jong-Sung
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2005년도 ICCAS
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    • pp.1972-1977
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    • 2005
  • In this work, an inverse dynamic control method is developed to enhance tracking performance of industrial robots, which effectively deal with the nonlinear dynamic interferential forces. In general, the DFF (Dynamic Feed-Forward) controller and the CTM (Computed-Torque Method) controller are used for dynamic control for industrial robots. We study on the practical issues for implementing these inverse dynamic controllers via simulations and experiments. We develop the dynamic models in two different ways. One is a model designed through Newton-Euler method for real time computation and the other is a model designed through SimMechanics for evaluating the developed controller via simulations. We evaluate the nominal performance and robustness of the controller via simulations and experiments using serial 4-DOF HyRoHILS (Hyundai Robot Hardware-In-the-Loop Simulation) system. The results show that the inverse dynamic controller is effective and practically useful for a real control structure.

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로봇 매니풀레이터의 치수 최적화 (Study on the dimension optimization of the robot manipulator with three links)

  • 조선휘;문홍기
    • 대한기계학회논문집
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    • 제12권4호
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    • pp.730-737
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    • 1988
  • 본 연구에서는 로봇 매니퓰레이터의 각 조인트 토오크를 구하고, 이를 최소자 승법에 의하여 각 링크의 길이를 최적화하였다. 이때 각 링크의 단면은 일정하며 따 라서 각 링크의 무게중심은 링크의 중앙에 있다고 보았다. 작업은 직선운동(C.P)으 로 하였고 이때의 소고 선도를 편의상 삼각형으로 하였다. 작업시간은 속도선도와 작업경로가 주어지면 구하여지고, 이를 등간격으로 나누어 매 순간마다의 조인트 토오 크를 구하였다. 이때 매 순간 기구학적 해석으로 조인트의 변위, 속도, 가속도를 구 하고 Newton-Euler 운동방정식을 이용하여 각 조인트 토오크를 구하였다.

영상 기반 자동 착륙용 멀티로터 시스템 설계 및 개발 (Design and Fabrication of Multi-rotor system for Vision based Autonomous Landing)

  • 김규범;송승화;윤광준
    • 한국인터넷방송통신학회논문지
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    • 제12권6호
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    • pp.141-146
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    • 2012
  • 본 논문에서는 영상 기반 자동 착륙 시스템 개발과 이 시스템을 사용하는 멀티로터 플랫폼 개발에 대해서 소개 한다. 멀티로터 플랫폼은 뉴턴 오일러 개념을 근간으로 하는 강체 운동 모델링을 하였고, LQR 제어 기법을 통한 제어기 튜닝 및 시뮬레이션을 하였다. 영상기반 자동 착륙 시스템은 멀터로터 시스템에 탑재된 단일 카메라를 사용하여 추가적인 임무장비 없이 증강 현실 알고리즘을 사용하여 마커를 탐지하고 정밀한 착륙을 유도하도록 GCS와 연동 코드를 구현 하였다.