• 제목/요약/키워드: Multi-DOF System

검색결과 91건 처리시간 0.028초

Parametric study of pendulum type dynamic vibration absorber for controlling vibration of a two DOF structure

  • Bur, Mulyadi;Son, Lovely;Rusli, Meifal;Okuma, Masaaki
    • Earthquakes and Structures
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    • 제13권1호
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    • pp.51-58
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    • 2017
  • Passive dynamic vibration absorbers (DVAs) are often used to suppress the excessive vibration of a large structure due to their simple construction and low maintenance cost compared to other vibration control techniques. A new type of passive DVA consists of two pendulums connected with spring and dashpot element is investigated. This research evaluated the performance of the DVA in reducing the vibration response of a two degree of freedom shear structure. A model for the two DOF vibration system with the absorber is developed. The nominal absorber parameters are calculated using a Genetic Algorithm(GA) procedure. A parametric study is performed to evaluate the effect of each absorber parameter on performance. The simulation results show that the optimum condition for the absorber frequencies and damping ratios is mainly affected by pendulum length, mass, and the damping coefficient of the pendulum's hinge joint. An experimental model validates the theoretical results. The simulation and experimental results show that the proposed technique is able be used as an effective alternative solution for reducing the vibration response of a multi degree of freedom vibration system.

The Application of Resettable Device to Semi-Active Tuned Mass Damper Building Systems for Multi-level Seismic Hazard Mitigation

  • Chey, Min-Ho
    • Architectural research
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    • 제14권3호
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    • pp.99-108
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    • 2012
  • An innovative multi-story Semi-Active Tuned Mass Damper (SATMD) building system is proposed to control seismic response of existing structures. The application of adding new stories as large tuned mass and semi-active (SA) resettable actuators as central features of the control scheme is derived. For the effective control of the structures, the optimal tuning parameters are considered for the large mass ratio, for which a previously proposed equation is used and the practical optimal stiffness is allocated to the actuator stiffness and rubber bearing stiffness. A two-degree-of freedom (2-DOF) model is adopted to verify the principal efficiency of the suggested structural control concept. The simulations for this study utilizes the three ground motions, from SAC project, having probability of exceedance of 50% in 50 years, 10% in 50 years, and 2% in 50 years for the Los Angeles region. 12-story moment resisting frames, which are modified as '12+2' and '12+4' story structures, are investigated to assess the viability and effectiveness of the system that aims to reduce the response of the buildings to earthquakes. The control ability of the SATMD scheme is compared to that of an uncontrolled and an ideal Passive Tuned Mass Damper (PTMD) building system. From the performance results of suggested '12+2' and '12+4' story retrofitting case studies, SATMD systems shows significant promise for application of structural control where extra stories might be added.

로봇을 이용한 다기능 상지 재활 시스템에 관한 연구 (A Study on the Multi-Purpose Rehabilitation System for the Upper Limb Using a Robot Manipulator)

  • 원주연;심형준;박범석;한창수
    • 한국정밀공학회지
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    • 제20권11호
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    • pp.171-179
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    • 2003
  • This paper presents a rehabilitation exercise system which utilizes a 6 DOF robot as a motion generator. This system was proposed for a stroke patient or a patient who has hemiplegia. A master-slave system was designed to exercise either paralysis or abnormal limb by using normal limb motion. The study on the human body was applied to calculate the motion range of elbows and shoulders. In addition, a force-torque sensor was applied to the slave robot to estimate the rehabilitation extent of the patient. Therefore, the stability of the rehabilitation robot could be improved. By using the rehabilitation robot. the patients could exercise by themselves without assistance. In conclusion, the proposed system was verified by computer simulations and system experiment.

Dynamic Analysis of Harmonically Excited Non-Linear Structure System Using Harmonic Balance Method

  • 문병영;강범수;김병수
    • Journal of Mechanical Science and Technology
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    • 제15권11호
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    • pp.1507-1516
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    • 2001
  • An analytical method is presented for evaluation of the steady state periodic behavior of nonlinear structural systems. This method is based on the substructure synthesis formulation and a harmonic balance procedure, which is applied to the analysis of nonlinear responses. A complex nonlinear system is divided into substructures, of which equations are approximately transformed to modal coordinates including nonlinear term under the reasonable procedure. Then, the equations are synthesized into the overall system and the nonlinear solution for the system is obtained. Based on the harmonic balance method, the proposed procedure reduces the size of large degrees-of-freedom problem in the solving nonlinear equations. Feasibility and advantages of the proposed method are illustrated using the study of the nonlinear rotating machine system as a large mechanical structure system. Results obtained are reported to be an efficient approach with respect to nonlinear response prediction when compared with other conventional methods.

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탄소 나노 튜브-팁 제작을 위한 다자유도 나노 정렬 시스템 개발 (Development of Multi-DOF Nano Aligner System for CNT-Tip)

  • 강경수;이준석;최재성;곽윤근;김수현
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.923-928
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    • 2004
  • AFM tip has been used for surface profiling with a fine resolution, but there is a barrier to improve its performance because of the low aspect ratio. Many researchers have solved this problem with attaching carbon nanotube (CNT) to Si-tip. In this paper, we proposed the aligner system that composed of dual type stage system, and these stages could attach a carbon nanotube to tungsten-tip in vacuum condition. We used tungsten tip instead of Si-tip because of its conductivity. The aligner system proposed in this paper has 10 degree-of-freedom that 3 in the first stage and 7 in the second stage. With picomotors and piezotube, the first stage has the resolution about several tens of nm and the second stage has a resolution about a nm. We experimented on characterization of Nano Aligner System and operated picomotors in SEM environment.

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Dynamic Analysis of Harmonically Excited Non-Linear System Using Multiple Scales Method

  • Moon, Byung-Young;Kang, Beom-Soo
    • Journal of Mechanical Science and Technology
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    • 제16권6호
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    • pp.819-828
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    • 2002
  • An analytical method is presented for evaluation of the steady state periodic behavior of nonlinear systems. This method is based on the substructure synthesis formulation and a MS (multiple scales) procedure, which is applied to the analysis of nonlinear responses. The proposed procedure reduces the size of large degrees-of-freedom problem in solving nonlinear equations. Feasibility and advantages of the proposed method are illustrated with the nonlinear rotating machine system as an example of large mechanical structure systems. In addition, its efficiency for nonlinear response prediction will be shown by comparison of other conventional methods.

강 뼈대 구조물의 다자유도 실시간 하이브리드 동적 실험 (Multi-DOF Real-time Hybrid Dynamic Test of a Steel Frame Structure)

  • 김세훈;나옥빈;김성일
    • 대한토목학회논문집
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    • 제33권2호
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    • pp.443-453
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    • 2013
  • 하이브리드 실험은 수치해석 모형과 물리적 부분구조 모형사이의 상호작용을 통하여 구조물의 거동을 예측하는 실험법이다. 본 연구에서는 지진하중 재하 시 1경간 2층 강 뼈대 구조물에 대한 다자유도 하이브리드 실험을 수행하고 유효성을 확보하는데 그 목적이 있다. 이를 위해 전용 하이브리드 수치해석 프로그램인 FEAPH을 개발하였으며, 최적화된 시스템을 구축하였다. FEAPH은 고정 반복법(Fixed iteration)과 병렬화(Parallelization) 기법을 적용하여 순차적 해석에서 발생되는 비효율적 연산을 개선하였다. 또한, 종전에 데이터 통신과 부분구조물과 해석프로그램간의 인터페이스를 간략화하여 하이브리드 시스템 구성을 최적화 하였다. 그 결과, 입력 가진시간(30초) 대비 약 10%의 실험시간이 소요되었다. 시스템의 신뢰성을 검증하고 선형실험과 강 뼈대 구조물의 동적거동을 예측하기 위해 비선형 실험을 수행하였으며 수치해석과의 변위응답이력은 거의 일치 하였다. 그러나 최대변위에 대한 응답은 다소 차이를 보였으며, 이는 재료 비선형성에 대한 해석상의 오차와 영구변형에 의해 발생한 것으로 판단된다. 따라서 적절한 재료 비선형 모델과 알고리즘의 개선이 이루어지면, 실시간 하이브리드 시스템은 구조물의 동적거동을 예측하는데 유용하게 활용될 것이며, 추후 진동대 실험을 대체할 수 있는 효과적인 실험 방법이 될 것으로 판단된다.

Dynamic and reliability analysis of stochastic structure system using probabilistic finite element method

  • Moon, Byung-Young;Kang, Gyung-Ju;Kang, Beom-Soo;Cho, Dae-Seung
    • Structural Engineering and Mechanics
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    • 제18권1호
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    • pp.125-135
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    • 2004
  • Industrial structure systems may have nonlinearity, and are also sometimes exposed to the danger of random excitation. This paper proposes a method to analyze response and reliability design of a complex nonlinear structure system under random excitation. The nonlinear structure system which is subjected to random process is modeled by finite element method. The nonlinear equations are expanded sequentially using the perturbation theory. Then, the perturbed equations are solved in probabilistic methods. Several statistical properties of random process that are of interest in random vibration applications are reviewed in accordance with the nonlinear stochastic problem.

광소자 정렬용 극초정밀 다축 위치 제어장치 개발 (Development of Multi-axis Nano Positioning Stage for Optical Alignment)

  • 정상화;이경형;차경래;김현욱;최석봉;김광호;박준호
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2004년도 추계학술대회 논문집
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    • pp.304-307
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    • 2004
  • As optical fiber communication grows, the fiber alignment become the focus of industrial attention. This greatly influence the overall production rates for the opto-electric products. We proposed multi-axis nano positioning stage for optical fiber alignment. This device has 3 DOF translation and sub nanometer resolution. This nano stage consist of 3 PZT-driven flexure stages which are stacked parallel. The displacement of it is measured with capacitance gauge and is controlled by computer-embedded main controller. The design process of flexure stage using FEM is proposed and the performance evaluation of this system is verified with experiments.

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모형 헬리콥터 정지비행제어에 관한 연구 (A Study on Hovering Flight Control for a Model Helicopter)

  • 심현철;이은호;이교일
    • 대한기계학회논문집
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    • 제18권6호
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    • pp.1399-1411
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    • 1994
  • A model helicopter has more versatile flight capability than the fixed-wing aircraft and it can be used as an unmaned vehicle in hazardous area. A helicopter, similar to other aircrafts, is an unstable, multi-input multi-output nonlinear system exposed to strong disturbance. So it should be controlled by robust control theories that can be applied to multivariable systems. In this study, motion equations of hovering are established, linearized and transformed into a state equation form. Various parameters are measured and calculated in other to obtain the stability derivatives in the state equation. Hovering flight controller is designed using the digital LQG/LTR(Linear Quadratic Gaussian/Loop Transfer Recovery) control theory. The designed controller is tested by the nonlinear simulations and implemented on an IBM-PC/386. Experiments were carried out on a model helicopter attached to the 3-DOF gimbal. The designed controller showed satisfactory hovering capability to maintain the hovering for more than 40 seconds.