• 제어로봇시스템학회논문지
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• 제5권2호
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• pp.220-227
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• 1999

The position control accuracy of a robot arm is significantly deteriorated when a long slender arm robot is operated at a high speed. In this case, the robot arm needs to be modeled as a flexible structure, not a rigid one, and its control system needs to be designed with its elastic modes taken into account. In this paper, the vibration control scheme of a one-link flexible manipulator using adaptive input shaper in conjunction with PID controller is presented. The robot consists of a flexible arm manufactured with a thin aluminium plate, an AC servo motor with a harmonic drive for speed reduction, an optical encoder and an accelerometer. On-line identification of the vibration mode is done using the pruned decimation-in-time FFT algorithm to estimate the parameter of the input shaper. Experimental results of the flexible manipulator with a PID controller and input shaper are provided to show the effectiveness of the advocated controllers.

• 한국소음진동공학회논문집
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• 제22권6호
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• pp.582-587
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• 2012

This paper presents a solution of the vibration reduction in the hollow shafts by using magentorehological( MR) elastomer. Proposed active damping structure is built by embedding the MR elastomers whose elastic modulus is controllable by an applied magnetic field. MR elastomers consist of synthetic rubber filled with micron-sized magnetizable particles. For reduction of vibration, dynamic damper of hollow shaft is designed by using MR elastomer and equipped in the hollow shaft for the application to drive shaft. Experiment results are shown through the experiments to confirm the effect of MR elastomer dynamic damper for vibration reduction. Thus, the designed damping structure can be applied to vibration absorber used in drive shafts as well as the propeller shafts.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2008년도 추계학술대회논문집
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• pp.278-279
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• 2008

• 한국정밀공학회지
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• 제16권12호
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• pp.126-132
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• 1999

The paper presents the modeling and optimal control for the reduction of transverse vibration of simply supported beam under a moving mass. The equations of motion are derived by using assumed mode method. The coriolis and centripetal accelerations are accommodated in the equations of motion to account for the dynamic effect of the traveling mass. In order to reduce the transverse vibration of the beam, an optimal controller with full state feedback is designed based on the linearized equations of motion. The optimal actuator locations are determined with the evaluation of an optimal cost functional defined by the worst initial condition with the trade-off of controlled mode performance. Numerical simulations are performed with respect to various velocities and different traveling masses. Even if the velocity of the traveling mass reaches to the critical speed which can cause the resonance of the beam, the controller with two piezoelectric actuators shows the excellent performance under severe time-varying disturbances of the system.

• Smart Structures and Systems
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• 제16권6호
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• pp.1003-1021
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• 2015

MR dampers have been proposed for the control of cable vibration of cable-stayed bridge in recent years due to their high performance and low energy consumption. However, the highly nonlinear feature of MR dampers makes them difficult to be designed with efficient semi-active control algorithms. Simulation study has previously been carried out on the cable-MR damper system using a semi-active control algorithm derived based on the universal design curve of dampers and a bilinear mechanical model of the MR damper. This paper aims to verify the effectiveness of the MR damper for mitigating cable vibration through a full-scale experimental test, using the same semi-active control strategy as in the simulation study. A long stay cable fabricated for a real bridge was set-up with the MR damper installed. The cable was excited under both free and forced vibrations. Different test scenarios were considered where the MR damper was tuned as passive damper with minimum or maximum input current, or the input current of the damper was changed according to the proposed semi-active control algorithm. The effectiveness of the MR damper for controlling the cable vibration was assessed through computing the damping ratio of the cable for free vibration and the root mean square value of acceleration of the cable for forced vibration.

• 한국항공우주학회지
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• 제50권11호
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• pp.791-800
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• 2022

능동 진동 제어 시스템(Active vibration control system, AVCS)을 이용하여 헬리콥터 기체의 능동 진동 제어 시 우수한 진동 제어 성능을 얻기 위하여서는 진동 상쇄 하중 발생기의 개수, 위치 및 하중 방향의 조합의 최적화가 중요하다. 따라서 고려 가능한 모든 하중 발생기의 조합에 대하여 헬리콥터 기체에 대한 AVCS의 진동 제어 성능을 조사하기 위해 Exhaustive 시험 기법을 적용한 AVCS 프레임워크를 구축하였다. 로터 진동 하중 해석, 기체 진동 응답 해석 및 AVCS 시뮬레이션 연구를 수행하기 위해 DYMORE II, MSC.NASTRAN 및 MATLAB Simulink 등 다양한 프로그램을 사용하였다. 이를 이용하여 비행 속도 158 knots의 UH-60A 헬리콥터에 대한 AVCS 적용을 위한 CRFG 조합을 최적화하였다. 최적의 CRFG 조합이 적용된 AVCS를 통해 UH-60A 헬리콥터의 4P 기체 진동 응답을 능동 제어한 결과, 기체의 주요 위치에서 4P 기체 진동 응답이 19.35~98.07%만큼 감소될 수 있었다.

• Smart Structures and Systems
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• 제13권2호
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• pp.281-303
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• 2014

In order to suppress the wind-induced vibrations of the Canton Tower, a pair of active mass driver (AMD) systems has been installed on the top of the main structure. The structural principal directions in which the bending modes of the structure are uncoupled are proposed and verified based on the orthogonal projection approach. For the vibration control design in the principal X direction, the simplified model of the structure is developed based on the finite element model and modified according to the field measurements under wind excitations. The AMD system driven by permanent magnet synchronous linear motors are adopted. The dynamical models of the AMD subsystems are determined according to the open-loop test results by using nonlinear least square fitting method. The continuous variable gain feedback (VGF) control strategy is adopted to make the AMD system adaptive to the variation in the intensity of wind excitations. Finally, the field tests of free vibration control are carried out. The field test results of AMD control show that the damping ratio of the first vibration mode increases up to 11 times of the original value without control.

• Smart Structures and Systems
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• 제18권1호
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• pp.93-115
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• 2016

A particle tuned mass damper (PTMD) system is the combination of a traditional tuned mass damper (TMD) and a particle damper (PD). This paper presents the results of an experimental and analytical study of the damping performance of a PTMD attached to the top of a benchmark model under wind load excitation. The length ratio of the test model is 1:200. The vibration reduction laws of the system were explored by changing some system parameters (including the particle material, total auxiliary mass ratio, the mass ratio between container and particles, the suspending length, and wind velocity). An appropriate analytical solution based on the concept of an equivalent single-unit impact damper is presented. Comparison between the experimental and analytical results shows that, with the proper use of the equivalent method, reasonably accurate estimates of the dynamic response of a primary system under wind load excitation can be obtained. The experimental and simulation results show the robustness of the new damper and indicate that the damping performance can be improved by controlling the particle density, increasing the amount of particles, and aggravating the impact of particles etc.

• 화약ㆍ발파
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• 제28권2호
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• pp.50-58
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• 2010

본 연구는 아직 국내에서 연구가 미비한 분야인 슬롯드릴링 공법에 대해 분석한 것이며 슬롯드릴링 공법을 공사현장에서 적용할 수 있는 이론적인 기반을 마련하고자 하였다. 본 연구는 슬롯드릴링 공법을 통해 진동저감의 가능성을 제안한다. 수치해석을 통해 슬롯드릴링의 유효제원 관해 크게 두 가지를 분석 하였다. 하나는 슬롯과 진원 사이의 거리에 따른 진동속도의 변화를 분석이며 다른 하나는 진동제어를 위한 적절한 크기의 슬롯너비와 슬롯높이를 찾고자 하였다. 결론적으로 진원과 슬롯사이의 거리가 멀어질수록 진동저감 효과가 감소함을 알 수 있었다. 그리고 슬롯제원의 변화에 따른 임의의 계측지점에서의 진동속도에 대한 영향도 확인할 수 있었다.

• 대한기계학회논문집A
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• 제37권1호
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• pp.25-30
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• 2013

군용 견마로봇차량은 전시 임무수행간 야지를 주행하게 되는데, 이때 발생하는 지속적인 충격에 의한 차체의 진동은 내부 구성품에 손상을 초래할 수 있다. 현재 차체 진동저감을 위한 제어의 수단으로 능동 또는 반능동 현가장치을 사용한 많은 연구가 진행 되고 있다. 본 연구에서는 기존의 반능동 현가장치와 더불어 $6{\times}6$ 차량의 회전형 현가장치와 독립적인 구동제어에 의한 진동저감 기법을 제안한다. 진동 제어기로는 스카이훅의 수정기법 중의 하나인 SH-ADD 를 적용하였다. ISO E 등급의 노면을 주행노면으로 선정하였으며, 시뮬레이션은 ADAMS Control 과 Matlab Simulink 를 연동하여 수행하였다. 야지에서의 내부장비의 피로누적에 초점을 두어 주행 제어조건에 따른 RMS 수치로서 결과를 비교 및 분석하였다.