• Title/Summary/Keyword: 능동진동제어 시스템

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Uncertainties and Control of a 3-DOF Active Vibration Isolation System (3자유도 능동형 제진 시스템의 불확실성과 제어)

  • Kim, Hwa-Soo;Pahk, Heui-Jae;Cho, Young-Man;Moon, Jun-Hee
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.16 no.12 s.117
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    • pp.1262-1271
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    • 2006
  • Using the physics-based model for the vibration isolation system, the model uncertainties are described. With the model including parameter perturbations, the robust controller to meet the robust performance and stability is designed through $\mu$-synthesis by DK-iteration. The order of controller is reduced by virtue of Hankel norm approximation technique to allow the efficient implementation in the real-time experimental environment without any performance degradation. The performance of the reduced $\mu$-controller is accessed in comparison with the original one. The experiments validate the superiority of the proposed control scheme against the model uncertainties and its applicability with varying payload.

A Study on Vibration Control Performance of Macpherson Type Semi-Active Suspension System (맥퍼슨 타입 반 능동 현가장치의 진동제어 성능 고찰)

  • Dutta, Saikat;Han, Chulhee;Lee, TaeHoon;Choi, Seung-Bok
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.26 no.2
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    • pp.157-164
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    • 2016
  • The paper studies a comparison analysis of semi-active control strategies for a Macpherson strut type suspension system consisting of MR(magneto-rheological) damper. As a first step, in order to formulate governing, a dynamic full model of a Macpherson strut is developed considering the kinematics. The nonlinear equation of motion of the strut is then linearized around the equilibrium point. A new adaptive moving sliding model controller is developed for fast response of the system. A newly proposed adaptive moving sliding mode control strategy is then compared with conventional sliding mode controller and skyhook controller. The comparison is made for two different types of road inputs; bump and random road profiles showing superior vibration control performance in time and frequency domains.

Advanced Railway Vehicle Technology using Smart Materials (지능재료를 이용한 차세대 철도차량기술)

  • 김재환;강부병;김형진;정홍채;최성규
    • Proceedings of the KSR Conference
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    • 2003.05a
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    • pp.712-717
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    • 2003
  • 지능 재료를 이용한 디바이스는 자연계에 존재하는 생명체와 같이 내.외부 환경 변화에 대응하여 스스로 변하는 능동적 기능을 갖고 있기 때문에 시스템 성능의 극대화 및 유지비용의 최소화를 가져오게 된다. 이러한 지능재료 기술은 지난 10여년 전부터 연구되었는데 대표적인 웅용을 보면, 산업, 항공, 교통, 운송 분야의 능동 소음 및 반능동 진동제어; 복합 재료 손상위치 탐지시스템, 손상구조 건전성 평가시스템, 교량, 저장탱크, 건물, 유조선, 대형 구조물의 건전성 평가 시스템; 초정밀 직진 안내기구, 나노 스테이지, 절삭오차 보정용 엑츄에이터, 초음파 회전모터, 지능유압 서보밸브, 변형 거울 등의 모터/엑츄에이터; 자동차 엔진 성능제어, 흡배기구 압력측정, 가속도 센서, 자이로센서, 에어백 센서, 타이어 센서 등의 지능 MEMS/NEMS 센서; electronic article 정찰, 도서태그, 비접촉 항공 운송물 분류 및 보안시스템, 전자 운전자 식별시스템, 광섬유 건물 보안 시스템, 지능 신경망 형상 인식 시스템 등의 보안 시스템; 지능항공기 구조물, 인공위성안테나, 헬리콥터 회전익 등의 형상제어가 있다. 본 논문에서는 지능재료 기술을 정리하고 차세대 철도차량 기술에 지금까지 적용한 예를 소개하며 향후 적용할 수 있는 분야들을 가능성 및 실용성 면에서 소개하고자 한다.

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Development of Power Amplifier for Piezoelectric Actuator and Control Algorithm Realization System for Active Vibration Control of Structures (구조물 능동진동제어를 위한 압전 작동기 구동 파워앰프와 제어 알고리즘 구현 시스템의 개발)

  • Lee, Wan-Joo;Kwak, Moon-K.
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.22 no.2
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    • pp.170-178
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    • 2012
  • This paper is concerned with the development of power amplifier and controller for piezoelectric actuator and sensor used in smart structures. Even though a high-voltage power amplifier is provided in the form of an operational amplifier, a very high DC voltage is still necessary as a power supply. In this study, we propose a low-cost design for the power amplifier including the DC power supply. We also need a controller on which a control algorithm will be mounted. In general, a digital signal processing chip is popularly used because of high speed. However, only commercial product is available for smart structure applications. In this paper, a controller consisting of a DSP and electronic circuits suitable for piezoelectric sensor and actuator pair is proposed. To validate the proposed controller with power amplifier, experiment on smart structure was carried out. The experimental results show that the proposed control system can be effectively used for smart structure applications with low cost.

Hybrid Control Model of MR Damper for Seismic Response Control of Adjacent Buildings (인접건축물의 지진응답 제어를 위한 MR 감쇠기의 복합제어 모델)

  • Kim, Gee-Cheol;Kang, Joo-Won;Chae, Seoung-Hun
    • Journal of Korean Association for Spatial Structures
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    • v.11 no.2
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    • pp.101-110
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    • 2011
  • Many researchers have attempted to apply semi-active control systems in the civil engineering structures. Recently, magneto-rheological(MR) fluid dampers have been developed. This MR damper is one of semi-active dampers as a new class of smart dampers. This paper discusses the application of MR damper for seismic response control of adjacent buildings subjected to earthquake. Here, a controllable damping force of MR damper that is installed between adjacent buildings is applied to seismic response control. A hybrid model combines skyhook and groundhook control algorithm so that the benefits of each can be combined together. In this paper, hybrid control model are applied to the multi degree of freedom system representative of buildings in order to reduce seismic response of adjacent buildings. And the performance of hybrid control model is compared with that of others. It was demonstrated that hybrid control model or adjacent buildings with MR damper was effective for seismic response control of two adjacent buildings reciprocally.

Design and Experimental Study for a Active Magnetic Bearing System by Using PID Control (PID 제어기를 이용한 능동형 자기베어링의 설계 및 실험적 동특성 연구)

  • Kyung, Jin-Ho;Kim, Jong-Sun;Lee, Hae
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1991.04a
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    • pp.83-89
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    • 1991
  • 본 연구에서는 5축 능동형 자기베어링 시스템에 대한 설계 및 제작 방법을 소개하고 모우드 변수 및 임계속도, 과도 및 정상상태에서의 응답 특성 등 관련 동특성을 실험으로 규명하였다. 자기베어링 제어방식은 PID 제어를 이 용하였고, air jet를 이용하여 회전체를 구동할 수 있도록 실험장치를 구성하 였다. 실험을 통하여 안정한 부상특성을 실현하였고, 1,2차의 임계속도를 통 과하여 10,000rpm이상이 회전속도에서도 안정하게 운전할 수 있었다.

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A Study on the Active Noise Cancellation System in a Vehicle Cabin Using the Weighting Factors of Control Error Path (제어오차계의 가중치를 이용한 차실내 능동소음제어 시스템 연구)

  • 홍석윤;허현무
    • Journal of KSNVE
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    • v.6 no.6
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    • pp.851-856
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    • 1996
  • The active noise cancellation system showing the effective convergence and stability has been studied by simplifying the controller structures using the weighting factors of control error path to the multi-channel filtered-x LMS algorithm which needs a lot of calculations and the performance has been verified experimentally. Besides, to implement the system performance in a vehicle cabin, experimental work for selecting the suitable numbers and positions of the microphones and speakers was accomplished. Effectively combining a TMS 320C 31 main processor conducting real number calculations and having various functions with other components, the purpose-built system board for active noise cancellation has been designed and with this board, car active noise cancellation system showing maximum stable 10dB noise reduction has been obtained at the car idling conditions above 3000rpm range.

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Application and Performance Evaluation of Helicopter Active Vibration Control System for Surion (헬리콥터 능동진동제어시스템의 수리온 적용 및 성능 분석)

  • Kim, Do-Hyung;Kim, Tae-Joo;Paek, Seung-Kil;Kwak, Dong-Il;Jung, Se-Un
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.6
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    • pp.557-567
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    • 2015
  • The most decisive factor of major sources of a helicopter is the main rotor system and the rotor-induced vibration is one of the technical challenges which should be resolved to ensure comfort for crews and passengers. Passive vibration reduction devices are adopted in conventional helicopters and several types of passive devices are also used in Surion. In recent years, foreign helicopter manufactures have increasingly applied the application of AVCS (active vibration control system) because of their superior performance with lower weight compared to passive device. In addition to weight reduction, AVCS has advantages maintaining its performance over aircraft configuration changes and flight condition changes. The technology demonstration program was performed in order to validate the performance of AVCS when applied to Surion, and optimization process for finding optimal configuration of sensors and actuators. Optimal configuration was produced using ground and flight test data, and its performance was evaluated and compared with flight test result.

항공기의 공탄성 제어를 위한 압전재료의 응용

  • 남창호;이근명
    • Journal of KSNVE
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    • v.6 no.1
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    • pp.11-19
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    • 1996
  • 지금까지의 항공기 날개에 공력 탄성학적 제어를 위해 압전재료를 작동기로 사용하는 연구는 아직은 완전하지 못하지만 실용화 가능성을 조사하기 위해 집중적인 투자가 행해지고 있다. 본 글에서 언급한 예 외에도 압전재를 이용 날개의 익형을 능동적으로 조절함으로써 천음속에서의 저항을 줄이기 위한 연구(transonic drag reduction with piezos), 압전재로 작동하는 제어면을 부착하여 헬리쿱터 블레이드 의 진동을 제어하기 위한 실험적 연구, 항공기 외부 장착물에 의해 발생되는 불안정 성을 제어하기 위한 압전작동기를 사용한 pylon decoupler 설계 등 다양한 분에에서 연구가 되고 있다. 하지만 아직까지는 제어에 필요한 충분한 제어력을 얻는 문제, 주 구조물과 압전재료의 강성도의 차이, 가용한 압전재의 실용화, 내구성 문제 등 항공 기에의 응용을 위한 새로운 재료의 개발이 요구되고 있다. 그리고 사용에 필요한 전력을 공급하는 문제는 지상에서 작동되는 시스템과는 달리 항공기에서는 해결해야 될 큰 문제점이며, 이에 대한 연구가 요구되고 있으며, 실용 가능성이 보일 경우 재료의 내구성, 제어 성능, 번개 등 외력에 대한 손상 예측 등 광범위한 연구가 이어 질 것으로 예측된다.

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An Analysis on Vibratory Loads Reduction using Individual Blade Control in Active Helicopter Rotors (지능형 헬리콥터 로터의 개별 블레이드 제어에 의한 진동하중 감소 해석)

  • Kim, Sung-Kyun;Shin, Sang-Joon;Kim, Tae-Seong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.6
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    • pp.496-502
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    • 2007
  • In the present paper, a new version of DYMORE, which is an analysis to solve a nonlinear multi-body dynamics problem, is used to simulate an Individual Blade Control (IBC) algorithm in order to reduce vibration in helicopter rotors. The Active Twist Rotor (ATR), in which Active Fiber Composites (AFC) are embedded, is utilized for IBC. The main purpose of the present investigation is to compare the analytical results with experiments and previous version of DYMORE. The experiments are performed at NASA Langley Transonic Dynamics Tunnel. According to the present result, it is observed that the correlation regarding the vibratory loads is improved.