• 대한기계학회논문집A
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• 제21권12호
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• pp.2179-2186
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• 1997

In this paper, the performance of a semi-active suspension system for a passenger car has been investigated. Alternative semi-active suspensions control laws has been compared via simulations. The control laws investigated in this study are : sprung mass velocity feedback control law, sky-hook damping control law, and state feedback control law. Simulation results show that a semi-active suspension has potential to improve ride quality of automobiles.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2006년도 춘계학술대회논문집
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• pp.831-836
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• 2006

In the process of accurate manufacture and measurement, it is necessarily required to isolate external or internal vibration due to external disturbance and internal actuators. The higher vibration isolation system gets damping around resonance, the better it is generally. This paper analyzes the performance of an existing passive air-spring for vibration isolation table by using experiment and simulation. Optimal design for a passive air spring can be obtained by tuning the size of the orifice. Also design for an active isolation system is carried out by applying PID controller and considering non-linearity of pneumatic characteristics with help of look-up table. We have developed the active vibration isolation table with the better isolation performance.

• 한국소음진동공학회논문집
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• 제12권12호
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• pp.950-955
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• 2002

The coupled finite/boundary element method is used in numerical analysis for acoustic radiation from the vibration of rectangular composite plate which is simply supported. This analysis is validated using the Wallace equation for an isotropic plate. Active control of sound fields has been tarried out using 3 pairs of piezoelectric sensor/actuator and a pair of viscoelastic material by Passive constrained layer damping treatment. The results show that the optimal placement of piezoelectric sensor/actuator and VE patch is required to control the sound fields from a vibrating composite plate.

• 한국소음진동공학회논문집
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• 제11권6호
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• pp.193-199
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• 2001

Active control of forced vibration of the cantilevered laminated composite plates using collocated piezoceramic sensor/actuator is analyzed numerically and verified experimentally for various fiber orientations. Impact on the stiffness and the damping properties is studied by varying stacking sequence of [$\theta$$_{4}$O$_{2}$90$_{2}$]s for the laminated composite plate. For the forced vibration control, the plate is excited by one pair of collocated PZT exciters in resonance and its vibrational response is suppressed by the other collocated PZT sensor/actuator using direct negative velocity feedback. It is shown that the active control of forced vibration is more effective for the smart laminated plate with higher modal damped stiffness(2ζ$\omega$/aup 2/) .

• 한국소음진동공학회논문집
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• 제19권7호
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• pp.667-672
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• 2009

This paper is concerned with the development of linear magnetic actuator for active vibration control. The newly developed linear magnetic actuator consists of permanent magnets and copper coils. On the contrary to the voice-coil type actuator, the linear magnetic actuator utilizes magnetic flux to generate the shaft movement. In this study, experiments on the prototype linear magnetic actuator were carried out to investigate its dynamic characteristics. Block and inertia forces generated by the actuator were measured. The experimental results show that the actuator can be used as both actuator and active tuned-mass damper. The linear magnetic actuator was attached to a cantilever as the active-tuned mass damper and active vibration control experiment was carried out. The experimental results show that the newly developed linear magnetic actuator can be effectively used for the active vibration control of structures.

• 소음진동
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• 제6권3호
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• pp.267-273
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• 1996

이 글은 소음 진동분야에 종사하는 분들에게 압전형 지능구조물을 소개하면서 소음 분야의 응용예 및 활용 가능성 그리고 앞으로의 과제들을 알리고자 한다. 지능 구조물이란 감지기(sensor)와 가진기(actuator) 그리고 제어기(control logic)가 구조물에 합해져서 능동적인 기능을 갖고 있는 것으로서 주위 환경의 변화를 감지하여 이에 대처하는 거동을 하는 구조물이다. 예를 들어, 기계적인 지능구조물은 그 위치 나 속도 또는 구조물의 강성도나 감쇠 성질을 변화시키는 구조물이다. 따라서 이러한 적응력을 갖춘 구조물은 많은 공학 분야에 큰 영향을 주고 있으며 소음제어 분야에 있어서도 큰 기대가 된다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 춘계학술대회논문집
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• pp.1333-1337
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• 2000

The flexural vibration of laminated composite beams with active and passive constrained-layer damping has been investigated to design structure with maximum possible damping capacity. The equations of motion are derived for flexural vibrations of symmetrical, multi-layer laminated beams. The damping ratio and modal damping of the first bending mode are calculated by means of iterative complex eigensolution method. This paper addresses a design strategy of laminated composite under flexural vibrations with active control.

• 한국지진공학회:학술대회논문집
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• 한국지진공학회 1999년도 춘계 학술발표회 논문집 Proceedings of EESK Conference-Spring
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• pp.196-201
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• 1999

In active control of structures the stroke of a Hybrid Mass Damper is the one of he main constraints of the system because there is limited installation space available in the structure. To design an optimal controller for a HMD system control objective are defined considering these constraints and effectiveness of H-infinity control method with bilinear transform that satisfies the defined objective is examined for the optimum efficiency. Numerical results show that the proposed H-infinity controller satisfies the constraints and provides optimal performance.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 추계학술대회논문집
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• pp.262-267
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• 2000

The flexural vibration of aluminum beams with active and passive constrained-layer damping has been investigated experimentally to design structure with maximum possible damping capacity. Piezoelectric film is used as sensor and piezoceramic as actuator for negative velocity feedback control. This paper shows the effectiveness of active constrained-layer damping treatment through experiment, and we have carried out an experiment to study effect of beam thickness.

• 항공우주시스템공학회지
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• 제15권1호
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• pp.7-18
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• 2021

반능동형 MR댐퍼 착륙장치는 MR유체가 환형 유로를 지날 때 유체감쇠력 및 자장 제어 감쇠력을 발생시키는 댐퍼이다. 환형 유로를 지나는 MR 유체의 경우 필연적으로 불완전 발달 유동이 발생하게 되어, 이는 유체 감쇠력을 포함하는 댐퍼 내력 계산에 오차를 발생시키는 원인이 된다. 이로 인해 댐퍼 구조적 파라미터 설계 및 제어 이득 선정이 부정확해지며, 착륙장치의 동특성 및 충격흡수성능 저하를 초래하게 된다. 본 논문에서는 MR댐퍼 환형 유로의 입구영역에서 발생하는 추가적인 감쇠력을 고려한 MR댐퍼 착륙장치의 수학적 모델을 유도하였다. 본 논문에서 유도한 수학적 모델링을 MR댐퍼 착륙장치의 설계 및 최적화 과정에 적용한다면 좀 더 정확한 내력 예측으로 우수한 성능의 MR댐퍼 착륙장치를 설계할 수 있을 것으로 판단된다.