• Defense and Technology
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• no.3 s.145
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• pp.17-25
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• 1991

Sting Ray는 현대의 첨단기술로 제작된 경어뢰로서, 완전히 디지털 컴퓨터 제어에 의해 작동한다. 항공기에 장착된 유도미사일과 그 기능을 견줄수 있는 최첨단 수중유도무기이며, 수중에서의 음파탐지 및 식별에 수반되는 각종 난관을 극복하였다. 수중에서의 음의 반사 및 굴절효과로 인해 복잡성이 가중된 잡음의 근원과 바닷물의 특성이 수시로 변화되는 상황에서 음향장치 사용을 결정하는 것은 매우 어려운 과제이나, Sting Ray는 이러한 어려운 환경을 극복할수 있도록 설계되었다. 또한 선박, 항공기 또는 헬기등 어디에서 발사되더라도 자율적으로 자체의 전술을 창조하는 Shaped Charge형 탄두는 어떠한 표적에도 치명적 피해를 줄수 있다

• The Proceedings of the Korean Institute of Illuminating and Electrical Installation Engineers
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• v.11 no.5
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• pp.53-61
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• 1997

본 연구에서는 편측식 선형 유도전동기(SLIM)를 구동원으로 한 지상 2차 방식의 반송설비시스템을 실험장치로서 구성하고, 이에 적용된 SLIM의 해석 및 설계을 위하여 Goodness factor와 가동자의 주행패턴을 고려하였다. 또한, 반송설비시스템의 추진구동원에 적용된 SLIM의 설계에 대한 타당성을 고찰하고자 유한요소법(FEM)에 의한 해석결과와 실험결과를 비교·분석하였으며, 이로부터 반송설비시스템은 물론 산업용 제어기기에 이르기까지 SLIM의 응용을 위한 기초자료를 제시할 수 있었다.

• Proceedings of the Korean Vacuum Society Conference
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• 2013.02a
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• pp.560-560
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• 2013

플라즈마 내의 전자 에너지 분포는 방전 특성 및 전자 가열 메커니즘에 대한 정보를 줄 수 있을 뿐만 아니라, 소자 생산 공정에서 공정 조건 제어 및 소자 품질 향상에 중요한 역할을 하는 변수이다. 그에 따라서, 반도체공정에서 널리 쓰이는 유도 결합 플라즈마 또는 용량성 결합 플라즈마 장치의 외부 변수에 따른 전자 에너지 분포 변화에 대한 연구가 많이 진행되어왔다. 본 연구에서는, 극판 전극이 인가된 유도 결합 플라즈마 구조에서 낮은 압력의 아르곤과 산소 기체 방전에 대하여 전자 에너지 분포를 측정하였다. 극판 전압만이 인가되었을 경우에는 두 개의 온도를 갖는 전자 에너지 분포를 측정하였으나, 소량의 안테나 전력을 인가할 경우 하나의 온도를 갖는 전자 에너지 분포를 측정할 수 있었다. 이러한 분포함수의 급격한 변화는 유도 결합 전기장과 용량성 결합 전기장의 혼재에 따른 전자 가열 효과이며, 극판에서의 전압, 전류 그리고 위상 측정을 통하여 전자 가열 메커니즘을 확인하였다.

• The Transactions of the Korean Institute of Power Electronics
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• v.9 no.3
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• pp.294-302
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• 2004

In this study, we developed the inverter system to control Induction motor for the vertically circulation parking facility. In the case of calling a pallet, a car parking space, we basically stoned conventional system's problems, pallet is uncontrollable to the fixed position and braking system was worn by forcer braking with remaining speed. Also, by appling to converter controller, added to power regenerative control function, we confirmed the reduce of power supply capacity and the energy saving effect according to increasing operation frequency. The validity of this system is verified by 55kw induction motor driving system. Via this study, the proposed system shows the efficient use of parking facility and good operation characteristics by implementing position and speed control effectively on condition of load and shows energy saying effect by power factor control for the vertically circulation parking facility operation.

• Journal of the Earthquake Engineering Society of Korea
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• v.9 no.2 s.42
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• pp.7-15
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• 2005

Numerical analysis model is proposed to predict the dynamic behavior of a single-degree-of-freedom structure that is equipped with hybrid base isolation system. Hybrid base isolation system is composed of friction pendulum systems (FPS) and a magnetorheological (MR) damper. A neuro-fuzzy model is used to represent dynamic behavior of the MR damper. Fuzzy model of the MR damper is trained by ANFIS (Adaptive Neuro-Fuzzy Inference System) using various displacement, velocity, and voltage combinations that are obtained from a series of performance tests. Modelling of the FPS is carried out with a nonlinear analytical equation that is derived in this study and neuro-fuzzy training. Fuzzy logic controller is employed to control the command voltage that is sent to MR damper. The dynamic responses of experimental structure subjected to various earthquake excitations are compared with numerically simulated results using neuro-fuzzy modeling method. Numerical simulation using neuro-fuzzy models of the MR damper and FPS predict response of the hybrid base isolation system very well.

• Journal of Aerospace System Engineering
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• v.15 no.3
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• pp.57-64
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• 2021

In the study, to minimize the error on guided control of the KV (Kill Vehicle) and to secure the hit-to-kill performance, a position accuracy inspection for the DACS (Divert and Attitude Control System) actuation system was proposed. The accuracy performance of the DACS actuation system is one of the most important factors in the interception of ballistic missiles. In order to validate actuation control accuracy of DACS system, an inspection item was set for position accuracy, and the inspection system was designed for DACS pintle. To measure the absolute position value of the DACS pintle, an external measurement system was developed using laser displacement sensors. The inspection system was designed so that it can be compared with the actuation command in real time. The proposed position accuracy inspection system can be inspected not only in a DACS system but also in missile system level. The position accuracy inspection was performed using the designed inspection system, and analysis of the inspection result.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.17 no.12
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• pp.1152-1160
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• 2007

In this paper we deal with a design of integral sliding mode controller to reject the disturbance force acting on the suspension system in the magnetically levitated system which is propelled by the linear induction motor. The control scheme comprises an integral controller which is designed for achieving zero steady-state error under step disturbances, and a sliding mode controller which is designed for enhancing robustness under plant uncertainties. A proper continuous design signal is introduced to overcome the chattering problem. The disturbance force produced by the linear motor is formularized by using a curve fitting of the experimental raw data. Computer simulations show the effectiveness of the designed integral sliding mode controller to reject the disturbance force.

• Journal of the Society of Naval Architects of Korea
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• v.37 no.3
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• pp.110-121
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• 2000

Gas heating, high frequency induction heating and laser heating can be used as the heat-source of line heating. Most of shipyards have been using the gas heating method for line heating. It is difficult to control the residual deformation of gas heating. High frequency induction heating is more feasible for the automation of line heating rather than the gas heating method since it is easy to control the magnitude of heat input. In this study, a numerical model of high frequency induction heating process is proposed for the application of the line heating. The simulation process of the induction heating is composed of the electromagnetic analysis, the heat transfer analysis, and the thermal deformation analysis.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.1
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• pp.35-42
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• 2020

Electromechanical Actuator(EMA) for flight vehicles generally serves to control the fin deflection angle or the thrust vector angle. This paper deals with design and development of EMA for both aerodynamic control and thrust vector control. In this paper, a novel compact EMA is proposed that can simultaneously control both the tail fin and the jet vane with one actuator and detach the jet vane after vertical launch and rapid turn of the flight vehicle so as to increase efficiency during flying to target. To do this, we designed the EMA using a push-push link mechanism and derived a mathematical model. The mathematical model is validated by comparing simulation result and experimental data. The performance and reliability of the proposed EMA have been verified through performance test, environmental test and ground test. The proposed EMA is expected to be useful as an EMA for flight vehicles because of its simple and compact structure, as well as its performance and reliability.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.13 no.12
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• pp.2685-2692
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• 2009

We propose pulsed magnetic stimulation below 30W by the AC(60Hz) switching control of leakage transformer primary which has some advantage of cost and size compared to a typical pulsed power supply. Pulse repetition rate is adjusted from 5Hz to 60Hz to control magnetic stimulation output. In this magnetic stimulation, a low voltage open loop control for high voltage discharge circuit is employed to avoid the HV sampling or switching and high voltage leakage transformer is used to convert rectified low voltage pulse to high voltage one. A ZCS(Zero Cross Switch)circuit and a DSP & FPGA are used to control gate signal of SCR precisely. The pulse repetition rate is limited by 60Hz due to the frequency of AC line and a high leakage inductance. The maximum magnetic stimulation output was obtained about 33W at pulse repetition rate of 60Hz, total 40, 80, 120, $160^{\circ}$, SCR gate trigger angle $90^{\circ}$ and total output.