• Proceedings of the Korean Vacuum Society Conference
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• 2011.08a
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• pp.91-91
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• 2011

본 개발에서는 초고속 복합 분자펌프 구동을 위한 디지털 구동장치를 설계 하였다. 초고속 모터구동을 위한 핵심제어 보드 설계 및 모듈을 설계하여 기본성능을 평가하였다. 또한 초고속 전동기 운전시 급가속 성능을 향상 하기 위해 홀센서에 의한 위치측정 오차를 최소화하는 관측기를 설계하여 모터제어기를 설계하여 고속회전 시험을 하였다. AMB 구동을 위한 전류제어기를 제작하여 성능시험을 하였다. AMB 구동을 위한 와전류식 변위센서 구동부를 설계 제작하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.41 no.1
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• pp.25-30
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• 2013

The piezoelectric-based hydraulic actuator is a hybrid device consisting of a hydraulic pump driven by piezoelectric stacks that is coupled to a conventional hydraulic cylinder via a set of fast-acting valves. Nowadays, such hybrid actuators are being researched and developed actively in many developed countries by requirement of high performance and compact flight system. In this research, operation principle and performance testing of the hybrid actuator were introduced. Output velocities have been measured in both loaded case and not loaded case and the blocking force also has been measured in external loaded case. The maximum velocity of the actuator is 53.3 mm/s, blocking force is 240.7 N and corresponding power output is 3.2 W.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.36 no.11
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• pp.1327-1334
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• 2012

This study shows the conformance-based design results of a fourth-order dynamic actuator showing a performance variation caused by variation in the components as well as aero-induced disturbances. The actuator comprises a BLDC motor, spur gear and worm gear assembly, and canard. The actuator performance was evaluated by using time-variant angle information of the canard. Based on the response surface models, critical system variables were screened using F-tests, and then, the performance was approximated as a function of the variables because it is difficult to determine the performance of a high-order dynamic system as a function of system variables through analytical approaches. In this study, the conformance of uncertain performance to the specification was defined as a probability measure. The design variables obtained by optimizing the measure can provide actuator performance conforming to the specifications considered, even though there is a variation in both the components and the aero-induced disturbances.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.11a
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• pp.227-230
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• 2008

Movable nozzle with a flexible seal have been used for Thrust Vector Control of the Solid Rocket Motor. The Hydraulic Testing Machine is consisted of Chamber, Actuator, Counterpotentiometer, and evaluates performance of Flexible seal for spring torque and axial compression. The qualification test of Flexible seal was conducted on design condition. A study fix up method of formulation, operation, inspection on Hydraulic testing machine.

• Journal of the Korean Geotechnical Society
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• v.34 no.2
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• pp.43-54
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• 2018

Underwater tracked vehicle is employed to perform underwater heavy works on saturated seafloor. When an underwater tracked vehicle travels on the seafloor, shearing action and ground settlement take place on the soil-track interface, which develops the soil thrust and soil resistance, respectively, and they restrict the tractive performance of an underwater tracked vehicle. Thus, unlike the paved road, underwater tracked vehicle performance does not solely rely on its engine thrust, but also on the soil-track interaction. This paper aimed at evaluating the tractive performance of an underwater tracked vehicle with respect to ground conditions (soil type, and relative density or consistency) and vehicle conditions (weight of vehicle, and geometry of track system), based on the soil-track interaction theory. The results showed that sandy ground and silty sandy ground generally provide sufficient tractions for an underwater tracked vehicle whereas tractive performance is very much restricted on clayey ground, especially for a heavy-weighted underwater tracked vehicle. Thus, it is concluded that an underwater tracked vehicle needs additional equipment to enhance the tractive performance on the clayey ground.

• Journal of the Korean Society of Propulsion Engineers
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• v.19 no.2
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• pp.17-28
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• 2015

In this paper, it is accomplished to design a control method for such an actuation system of simplified ON/OFF mechanism with actuation command limit. First of all, based on experimental data, the modeling works for nonlinear/linear actuation dynamics are performed, which are govern by PWM command as a control input. Using the linearized model, a classical PI control method is designed to satisfy the aimed control performance requirements, and a control algorithm is proposed to realize the required control performance in the effective control region through resolving the issue for the PWM command limit which reduces the control performance. Finally, through control simulations, the design method is verified and the corresponding control performance improvement is evaluated.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.47 no.2
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• pp.153-160
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• 2019

Electro-mechanical actuator system for aircraft has advantages in compactness and its lightweight, compared to the hydraulic actuator system. Hinge line actuator has low air resistance and is suitable for special purpose such as stealth. This paper describes design contents of 10,000 lbf-in class dual redundant hinge line electro-mechanical actuator system for performance test. The control structure was designed to minimize impact of torque fighting. A mathematical model is proposed to analyze and validate the performances of actuator by comparison with experiment results.

• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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• 2009.06a
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• pp.122-122
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• 2009

최근 PC의 성능이 향상되면서, 고성능의 전원공급 장치가 요구되고 있다. 특히 CPU에 대전력을 공급하는 싱크로너스 벅 컨버터는 파워 MOSFET을 구동하기 위해 별도의 구동 IC가 필요하다. 본 논문은 adaptive 지연을 이용하여 파워 MOSFET을 구동하는 싱크로너스 벅 구동 IC를 설계하였다. 고정밀도의 밴드캡 기준회로와 비교기를 이용하여 30 ns의 adaptive 지연을 생성하며, 전력소모를 줄이기 위해 저전압에서 동작하는 UVLO(under voltage lock out)를 설계하였다. 또한 상단 파워 MOSFET을 구동하기 위하여 부트스트랩 방식을 이용하며, 부트스트랩 다이오드를 IC 내부에 내장하여 컨버터의 설계비용을 줄였다. 설계한 구동 IC의 동작 전압 범위는 8 V - 15 V이며, 출력 전류는 최대 2A이다. 싱크로너스 벅 구동 IC는 $0.5\;{\mu}m$ BiCMOS(Bipolar-CMOS) 공정 파라미터를 사용하여 설계되었으며, 시뮬레이션은 Cadence사의 Spectre를 이용하였다.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2007.06a
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• pp.445-448
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• 2007

소형 LD 구동 장치를 개발하고, 그 성능을 평가하였다. 개발된 장치는 사용 및 이동이 편리하도록 소형으로 제작되었으며, 안정적인 LD의 구동을 위해 AGC(Auto Gain Control) 및 APC(Auto Power Control)를 적용하였다. 개발된 장치의 LD구동전류 안정도는 $100{\mu}AmA$ 이내로 레이저 광 출력 안정도는 0.07mW이하로 안정된 구동 성능을 나타내었다.

• Journal of Power System Engineering
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• v.14 no.2
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• pp.22-27
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• 2010

본 논문은 유한체적법에 근거한 CFD 분석기법을 이용하여 증기 이젝터의 성능에 대하여 구동노즐의 기하학적 형상에 따른 영향을 조사하였다. 구동노즐의 직경비를 변화시키고 또한 직경비를 일정하게하고 구동 노즐의 위치를 변화시키면서 최적의 조건을 조사하였다. 연구 결과 이젝터의 성능은 구동노즐의 직경과 노즐의 출구 위치에 의해 좌우됨을 확인하였다. 일정 노즐 면적비에 대하여 노즐 목 직경이 감소함에 따라 혼입율이 증가하는 것을 확인하였고 일정 노즐 목 직경에 대하여 면적비의 증가는 혼입율의 감소의 원인이 된다는 것을 확인할 수 있었다. 또한 혼입율은 노즐의 출구 위치에 따라 영향을 받는다는 것도 확인하였다. 혼입율은 노즐 출구의 위치가 이젝터의 상류로 이동할수록 증가하고 그 위치는 이젝터의 일정단면적부 직경(D)에 대하여 0.4D일 때 최적의 성능을 보였다.