• 제목/요약/키워드: actuation system

검색결과 336건 처리시간 0.026초

하이브리드 스마트 구조물의 진동 제어 (Vibration Control of Hybrid Smart Structures)

  • 박동원;박용군;박노준;최승복
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 1996년도 춘계학술대회논문집; 부산수산대학교, 10 May 1996
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    • pp.130-135
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    • 1996
  • This paper presents a proof-concept investigation on the active vibration control of two hybrid smart structures (HSSs). The first one is consisting of a piezoelectric film (PF) actuator and an electro-rheological fluid(ERF) actuator, and the other is featured by a piezoceramic (PZT) actuator and a shape memory alloy (SMA) actuator. For the PF/ERF hybrid smart structure, both the increment of the damping ratios and the suppression of the tip deflections are evaluated in order to demonstrate control effectiveness of the PF actuator and ERF actuator and the hybrid actuation. For the PZT/SMA hybrid smart structure, the PZT actuator takes account of the high frequency excitation, while the SMA actuator exerts large vibration control force. The experimental results exhibit superior abilities of the hybrid actuation systems to tailor elastodynamic responses of the HSS rather than a single class of actuation system alone.

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고장에 강인한 구형 3자유도 모듈에 관한 기구학적 해석 (Kinematic Analysis of Fault-Tolerant 3 Degree-of-Feedom Spherical Modules)

  • 이병주;김희국
    • 대한기계학회논문집
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    • 제18권11호
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    • pp.2846-2859
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    • 1994
  • This work deals with kinematic analysis of fault-tolerant 3 degree-of-freedom spherical modules which have force redundancies in its parallel structure. The performance of a redundantly actuated four-legged module with no actuator failure, a single actuator failure, partial and half failure of dual actuator are compared to that of a three-legged module, in terms of maximum force transmission ratio, isotropic characteristics, and fault-tolerant capability. Additionally, a system with an excess number of small floating actuators is considered, and the contribution of these small actuators to the force transmission and fault-tolerant capability is evaluated. This study illustrates that the redundant actuation mode allows significant saving of input actuation effort, and also delivers a fault tolerance.

기포형성에 의한 마이크로 액추에이터의 구동기구 해석 (Analysis on Actuation Mechanism of Micro Actuator by Bubble Formation)

  • 오시덕;승삼선;곽호영
    • 대한기계학회논문집
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    • 제19권2호
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    • pp.418-426
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    • 1995
  • A bubble-powered microactuator is designed conceptually. And the actuation mechanism due to bubble growth and collapse is studied numerically and analytically. In this analysis, it is estimated that the time lag for bubble formation on micro line heater, the duration of the bubble growth and collapse and the pressure change in actuator due to the bubble evolution. Based on these calculations, the actuator control scheme is visualized. This actuator may be applicable to the system which needs to pump liquid correctly and regularly.

잉여구동을 지닌 4절 기구에서의 강성효과에 대한 해석 (Stiffness Analysis in a Redundantly Actuated Four-Bar Mechanism)

  • 이병주
    • 대한기계학회논문집
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    • 제18권4호
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    • pp.846-855
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    • 1994
  • An effective stiffness, analogous to that of a wound spring, can be created by antagonistic redundant actuation of general closed-chain mechanisms. The qualitative and quantitative characteristics of the effective stiffness are investigated through a Four-bar mechanism, and a load distribution method is introduced which simultaneously guarantees the required system motion and the effective stiffness of the Four-bar mechanism. Furthermore, a simulation is performed to understand the inter-relationship among the effective stiffness, the Four-bar geometry, and the actuation effort. Based on this analysis, the Four-bar synthesis problem for effective stiffness generation is discussed.

TVC 구동력을 고려한 75톤급 엔진 정적 구조 해석 (Static Structural Analysis of 75 tonf-class Engine with TVC actuation force)

  • 유재한;;김옥구;전성민;정은환
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.913-914
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    • 2017
  • 액체로켓엔진 개발 과정에서 중량을 절감하고 구조 신뢰성을 증가시키기 위해서는 엔진 시스템에 대한 구조 해석이 필요하다. 발사체는 비행 중 자세제어를 위해 엔진의 TVC (thrust vector control) 구동기의 변위를 변화시켜 연소기를 회전하여 추력의 방향을 제어한다. 본 연구에서는 연소기 김발을 하는 75톤급 액체 로켓 엔진에 대하여 TVC 구동 전/후의 정적 구조 해석을 수행하고 비교하였다.

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단일 DC-Link 전류 계측만을 이용한 BLDC 구동시스템의 디지털 전류 제어 (A Digital Current Control using Single DC-Link Current Sensing of BLDC Actuation Systems)

  • 한봉수
    • 한국군사과학기술학회지
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    • 제22권1호
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    • pp.72-80
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    • 2019
  • In this paper, we propose a digital DC-Link current control approach for BLDC actuation systems. The proposed approach consists of the following two components: first, DC-Link current measurement with sampling instances synchronized with PWM frequency, and second, current control using single DC-Link current rather than three phases current of a motor. The proposed method proved its performance through experiments and simulation. The results showed that the control performance are increased compared with the BLDC actuation system which does not use current control.

마이크로 로봇 작동 성능 향상을 위한 FEM 기반의 전자석 배치 베이지안 최적화 (FEM-based Bayesian Optimization of Electromagnet Configuration for Enhancing Microrobot Actuation)

  • 권혁진;손동훈
    • 로봇학회논문지
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    • 제19권1호
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    • pp.45-52
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    • 2024
  • This paper introduces an approach to enhance the performance of magnetic manipulation systems for microrobot actuation. A variety of eight-electromagnet configurations have been proposed to date. The previous study revealed that achieving 5 degrees of freedom (5-DOF) control necessitates at least eight electromagnets without encountering workspace singularities. But so far, the research considering the influence of iron cores embedded in electromagnets has not been conducted. This paper offers a novel approach to optimizing electromagnet configurations that effectively consider the influence of iron cores. The proposed methodology integrates probabilistic optimization with finite element methods (FEM), using Bayesian Optimization (BO). The Bayesian optimization aims to optimize the worst-case magnetic force generation for enhancing the performance of magnetic manipulation system. The proposed simulation-based model achieves approximately 20% improvement compared to previous systems in terms of actuation performance. This study has the potential for enhancing magnetic manipulation systems for microrobot control, particularly in medical and microscale technology applications.

Mechanically Modulated Actuators and Branched Finger Detectors for Nano-Precision MEMS Applications

  • Cho, Young-Ho;Lee, Won-Chul;Han, Ki-Ho
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2002년도 ICCAS
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    • pp.39.1-39
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    • 2002
  • We present nanoactuators and nanodetectors for high-precision Micro Electro Mechanical System (MEMS) applications. Major technical difficulties in the high-precision MEMS are arising from the fabrication uncertainty and electrical noise problems. In this paper, we present high-precision actuators and detectors, overcoming the technical limitations placed by the conventional MEMS technology. For the nano-precision actuation, we present a nonlinearly modulated digital actuator (NMDA). NMDA composed of a digital microactuator and a nonlinear micromechanical modulator. The nonlinear micromechanical modulator is intended to purify the actuation errors in the stroke of the digital a...

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카본나노튜뷰/전도성 폴리머 복합재 엑츄에이터의 전압-변형률 관계식 (An Approximate Description of Strain-Voltage Relationships for SWNTs/Conducting Polymer Composite Actuator)

  • ;김철
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2004년도 추계학술발표대회 논문집
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    • pp.9-14
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    • 2004
  • An approximate relationship of the strain and applied potential was derived for SWNTs and conductive polymer composite actuator. During the deriving process, we used an electrochemical system to model the electromechanical actuation of the composite film. This relationship can give us a direct understanding to the actuation of a nanoactuator

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위성 추진시스템의 추력제어밸브 작동에 따른 추진제 비정상 유동 특성 (Transient Flow Behavior of Propellant with Actuation of Thrust Control Valve in Satellite Propulsion System)

  • 김정수;한조영;최진철
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집E
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    • pp.294-298
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    • 2001
  • Satellite propulsion system is employed for orbit transfer, orbit correction, and attitude control. The monopropellant feeding system in the low-earth-orbit satellite blowdowns fuel to the thrust chamber. The thrust produced by the thruster depends on fuel amount flowed into the combustion chamber. If the thruster valve be given on-off signal from on-board commander in the satellite, valve will be opened or closed. When the thrusters fire fuel flows through opened thruster valve. Instantaneous stoppage of flow in according to valve actuation produces transient pressure due to pressure wave. This paper describes transient pressure predictions of the KOMPSAT2 propulsion system resulting from latching valve and thrust control valve operations. The time-dependent set of the fluid mass and momentum equations are calculated by Method of Characteristics (MOC).

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