• 조명전기설비학회논문지
• /
• 제18권2호
• /
• pp.110-114
• /
• 2004

본 논문에서는 직선형 피스톤 액추에이터의 해석을 위해서 패러데이 법칙으로부터 기본 방정식을 유도하였고, 이를 바탕으로 소형, 경량, 고속 응답을 요구하는 시스템에 응용될 수 있는 실험적 자료를 얻었다. 본 논문에서는 자계로부터 일반적으로 구할 수 있는 전자기력을 기계 방정식과 결합하여 에너지 변환 이론에 의한 직선형 피스톤 액추에이터의 운동시 플런저의 동특성을 구하였다. 이러한 기존의 방법들을 구조적으로 단순화하면서 용수철의 탄성력을 활용하여 시스템에 적용할 수 있는 직선형 피스톤 액추에이터(Serial Piston Actuator, SPA)를 제안하고, 소규모 직선형 변위를 요구하는 시스템에서 유(공)압식 피스톤을 대치하거나 호환할 수 있는 목적을 가지며, 추후 이와 관련한 연구에 참고될 수 있는 실험용 모델을 구현하고 이를 해석하였다.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2009년도 추계학술대회 논문집
• /
• pp.292-298
• /
• 2009

This paper investigates the control performance of the proposed hybrid mount system for vibration isolation table. The hybrid mount system consists of an air spring as a passive device and a PZT stack actuator as an active device in series. The feasibility of the PZT stack actuator as an active actuator was examined through the simple experiments. After that, a series of numerical simulations were carried out to evaluate the control performance of the proposed hybrid mount system. The equations of motion of the table with a set of hybrid mount systems consisting of four devices are derived. The air spring is considered as a 1 spring and 1 dashpot elements, and PID control algorithm is adopted to estimate the control force. The results of the numerical simulations presents that the proposed hybrid mount system could be the promising control system for vibration isolation table.

• 융합보안논문지
• /
• 제7권2호
• /
• pp.145-154
• /
• 2007

본 논문에서는 유도무기체계의 구동장치 기술에 대한 사항과 발전방향에 대해 연구하였다. 유도무기체계의 구동장치로는 일반적으로 유 공압 및 전기모타 구동장치가 많이 사용되었으나 근래에는 작은 동력이 요구되는 소형 전술용 유도탄의 구동장치를 제외하고는 대부분 경우에 출력 대 무게비가 높은 유압구동장치가 사용되어 왔다. 그러나 최근에는 유도탄의 높은 기동성 혹은 반응성 요구와 함께 신소재를 이용한 자성재료들의 개발, 제어기술 및 동력전자 기술의 발달, 디지털화 또는 집적화 등 구동장치 관련 기술의 발전도 두드러져 구동장치의 기술수준과 설계개념 등이 빠른 속도로 변화하고 있다. 따라서 본 연구를 통해서 차세대의 유도무기체계 구동장치의 설계기준과 구성, 특성 및 세부기술의 발전방향 명확히 제시하였다.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 2004년도 ICCAS
• /
• pp.291-295
• /
• 2004

New valve driving system to control for the best volumetric efficiency at each load of an internal combustion engine within one engine cycle has been developed. The system needs to reduce pumping loss that cause by throttle valve during the intake valve is opened. In this system the intake valve is driven by a linear DC electromagnetic actuator which is controlled by personal computer. The result is compared both installed and uninstalled actuator into the cylinder head. By both of experimental and numerical calculation, the responsibility of the valve driving system to the engine speed was examined

• Journal of Electrical Engineering and Technology
• /
• 제3권3호
• /
• pp.401-407
• /
• 2008

The dynamic model and displacement control of piezoelectric actuators, which are commercially available materials for managing extremely small displacements in the range of sub-nanometers, are presented. Piezoceramics have electromechanical characteristics that transduce energy between the electrical and mechanical domains. However, they have hysteresis between the input voltage and output displacement, and this behavior is very demanding and complicated. In this paper, we propose a method of designing the control algorithm, and present the dynamic modeling equations that represent the hysteretic behavior between input voltage and output displacement. For this process, the piezoelectric actuator is treated as a second-order linear dynamic system and system constants are determined by the system identification method. Also, a classical PID controller is designed and used to regulate the output displacement of the actuator. To evaluate the performance of the proposed method, numerical simulation results are presented.

• 한국해양공학회지
• /
• 제16권4호
• /
• pp.61-69
• /
• 2002

In the actual control systems, there exist many kinds of restrictions or nonlinearities. However, due to the nonlinearities in actuators and sensors, the designed controller may not be applicable in some practical situations. One such nonlinearity is amplitude saturation in actuators. Although sometimes it may be ignored, in other cases failure to consider actuator saturation may severely degrade closed-loop system performance and even lead to instability. On the other hand, limiting the controller gain to avoid saturation sacrifices control effort and may lead to loss of performance. Consequently, in some cases, the actuator saturation must be explicitly taken into account to ensure desired performance. However, in this paper, an anti-windup control system design method is introduced to suppress the windup due to the amplitude saturation of the actuator. The proposed control system has very simple design process and guarantees the good control performance. The validity of the proposed control system will be shown by comparing with the results of a reported paper.

• 대한기계학회논문집A
• /
• 제27권3호
• /
• pp.472-477
• /
• 2003

A piezo-actuator is an important component for an E-beam lithography system. But it is very difficult to model its characteristics due to nonlinearities such as hysteresis and creep, to the input voltage. In this paper, one-axis micro stage with a piezo-actuator is modeled including the nonlinear properties. Hysteresis and creep are modeled as the first order differential equation and a time-dependent logarithmic function, respectively. The dynamic motion of the stage is also modeled as a mass-spring-damper system and the parameters are determined by utilizing the system identification technique. The simulation tool for a micro stage is constructed using the commercial software and its simulation results are compared with the experimental data.

• 한국공작기계학회:학술대회논문집
• /
• 한국공작기계학회 2003년도 추계학술대회
• /
• pp.227-232
• /
• 2003

As the most precision equipment requiring very strict vibration environment are vulnerable to the surrounding vibration condition, they adapt the passive or active vibration isolation system. When it comes to the passive isolation system, the resonance of the isolation system causes excessive resonance response, and finally results in the degrade the equipment performance. This paper deals with the active control method to control this resonance induced response, and includes the experiment on the active control for controlling the resonance response on the table against the excitation of the same frequency with the natural frequency of the isolation system. The electromagnetic actuator was designed and the control effect was verified by the experiment. The experiment showed that the electromagnetic actuator is effective for controlling the low frequency isolation resonance response of the precision equipment.

• 대한기계학회논문집A
• /
• 제25권3호
• /
• pp.478-485
• /
• 2001

A dynamic load simulator(DLS) which can reproduce on-ground the aerodynamic hinge moment of control surface is an essential rig for the performance and stability test of aircraft actuation system. By setting up load actuator as counter acting with the control surface driving actuator and designing an appropriate force control system for load actuator, DLS can be mechanized. Obtaining an accurate mathematical model for the DLS is the first step to successfully design an aerodynamic load replicati on system. Two theoretical models are presented and tested for their validities with the experimental results, which turns out to be not successful. An alternative way of using system identification approaches in investigated to develop a good nominal model for DLS dynamics, and suitable uncertainty bounds for this nominal model are proposed with the consideration of experimental results.

• Journal of Magnetics
• /
• 제16권2호
• /
• pp.120-124
• /
• 2011

The design of an air compressor-driving quadratic linear actuator in a fuel cell BOP system is studied using orthogonal techniques. The approach utilizes an orthogonal array for design of 'experiments', i.e. the scheme for numerical simulations using a finite element method. Eco-friendly energy is increasingly important due to the depletion of fossil fuels and environmental pollution. Among the new energy sources, fuel cell is spotlighted as renewable energy because it produces few dusts. The air compressor performance is directly related to the efficiency of the fuel cell BOP system has high power consumption. In this paper, an optimized technique using an orthogonal matrix is applied to the design problem to improve the performance of quadratic linear actuator.