• Transactions of the Korean Society of Automotive Engineers
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• v.22 no.1
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• pp.65-70
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• 2014

An Integrated Dynamics Control system with four wheel Steering (IDCS) is proposed and analysed in this study. It integrates and controls steer angle of front and rear wheel simultaneously to enhance lateral stability and steerability. An active front steer (AFS) system and an active rear steer (ARS) system are also developed to compare their performances. The systems are evaluated during brake maneuver and several road conditions are used to test the performances. The results showed that IDCS vehicle follows the reference yaw rate and reduces side slip angle very well. AFS and ARS vehicles track the reference yaw rate but they can not reduce side slip angle. On split-${\mu}$ road, IDCS controller forces the vehicle to go straight ahead but AFS and ARS vehicles show lateral deviation from centerline.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2011.04a
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• pp.206-211
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• 2011

In this paper, a control algorithm for the improvement of yaw and velocity stability of electrical vehicle with two or four in-wheel motors is proposed. The vehicle is modeled with independently operative in-wheel motor wheels. Different frictions on the wheels are regarded as disturbances, which causes driving instability. In this situation the proposed algorithm enables stabilizing the yaw motion and velocity of vehicle simultaneously. The proposed PID controller is composed with two techniques, which enhance the disturbance reject and point tracking performances. One is nonlinear gain function and the other one is improved integral controller operating as time based weight function. Simulation is conducted to reveal its efficient performance.

• Transactions of the Korean Society of Automotive Engineers
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• v.13 no.1
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• pp.83-89
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• 2005

This paper presents vehicle stability control algorithm based on 3-DOF vehicle model. The brake control inputs have been directly derived from the sliding control law based on a three degree of freedom plane vehicle model with differential braking. The simulation has performed using a full nonlinear 3-dimensional vehicle model and the performance of the controller has been compared to that of a direct yaw moment controller. Simulation results show that the proposed controller can provide a vehicle with better performance than conventional controller with respect to brake actuation without compromising stability at critical driving conditions.

• Proceedings of the KIEE Conference
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• 2007.07a
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• pp.1591-1592
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• 2007

본 논문에서는 상태궤환을 이용한 철도차량의 능동조향을 위한 제어기법에 대해 다루었다. 능동조향은 곡선부 주행시 발생되는 승차감 저하 및 차륜/레일의 마모, 소음을 줄이고 고속주행을 위한 조향성능 및 주행안정성을 확보하기 위한 기술이다. 논문에서 사용된 제어 방법은 반대차(Half Bogie) 차량모델을 기초로 측정된 휠-레일의 횡변위(Lateral Displacement) 와 요각(Yaw Ang;e)정보를 토대로 휠에 요모멘트를 제어하였으며 시뮬레이션을 통해 제안한 방법에 대한 성능을 검증하였다.

• Proceedings of the Korea Information Processing Society Conference
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• 2012.11a
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• pp.1300-1303
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• 2012

최근 친환경적이고 에너지 효율이 우수한 LED 조명에 대한 관심이 증가함에 따라 현재 학교 조명으로 사용하고 있는 형광등을 대체하고 있다. 형광등은 점멸빈도가 높으면 수명이 단축되며 상황에 따라 조명 환경을 동적으로 재구성하기에 용이하지 않은 단점을 가진 조명장치이다. 이와 달리 LED는 광원의 다양한 조합을 통해 정밀한 제어가 가능하여 상황에 따라 적합한 조명 환경을 제공함으로써 재실자의 시각적 쾌적성 및 작업 능률 향상 등의 효과를 가져온다. 본 논문에서는 교실 환경을 대상으로 요일 및 시간, 교과목 종류 등의 스케쥴 정보와 교사의 위치 및 행위를 기반으로 각 상황에 적합한 최적의 조명 환경을 제공하여 학습 능률을 향상시키기 위한 상황인지기반의 LED조명제어시스템을 개발한다. 제안한 시스템의 성능 평가를 위해 교실 환경 테스트베드를 구축하고 조명 환경 지표를 이용하여 교실 내 조명장치의 색온도, 조도를 제어한다.

• Proceedings of the Korea Information Processing Society Conference
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• 2013.05a
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• pp.299-300
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• 2013

본 논문은 진공흡착방식을 이용한 벽오르는 로봇에 탑재하기 위한 임베디드 시스템의 설계와 영상처리 알고리즘의 구현에 관한 연구이다. 벽로봇은 안정적인 부착과 이동성을 기반으로 벽면에서의 위험 요인 발견과 지능적인 처리를 위해 영상처리가 가능하고 원격의 스마트 단말기와 실시간 통신이 가능한 환경을 구축하였으며 이상 물질을 탐지하기 위해 색상성분을 정규화하고 특정객체를 탐지 후 영상을 전송하는 방법을 구현하였다. 이러한 기능은 무인로봇을 이용해 위험한 벽 환경에서의 균열이나 이상 원인을 지능적으로 탐색하는 분야에 응용 가능하다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.32 no.3
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• pp.88-94
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• 2004

The KSR-III rocket is a liquid propellant sounding rocket and thrust vector control actuators and cold gas thrusters are used to control pitch and yaw, roll attitude respectively during thrusting phase. In this paper, the structure of designed attitude controller and gain scheduling, results of stability analysis for KSR-III rocket are presented. The attitude controller is implemented with flight software in the domestically developed INS and successfully performed its function in the flight test. The flight data are coincident with simulation results.

• Proceedings of the KSME Conference
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• 2007.05a
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• pp.921-926
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• 2007

A dynamic system under random disturbance is considered in the study. In order to control the system efficiently, proper reduction of system dimension is indispensible in design stage. The reduction method using component cost analysis in conjunction with stochastic analysis is proposed for the control of a system. System response is obtained in terms of dynamic moment equation via Fokker-Plank-Kolmogorov(F-P-K) equation. The dynamic moment response of the system under random disturbance are reduced by using of deterministic version of component cost analysis. The reduced system via proposed "stochastic component cost analysis" is successfully implemented for dynamic response and shows remarkable control performance effectively utilizing "stochastic controller" in physical time domain.

• Journal of the Institute of Electronics Engineers of Korea TE
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• v.42 no.4
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• pp.47-52
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• 2005

In this paper, the genetic algorithm is used to design a fixed order square decoupling $H_{\infty}$ controllers based on the Two-Degree-of-freedom standard model. The proposed decoupling $H_{\infty}$ controller which is minimizes the maximum energy in the output signal is designed to reduce the coupling properties between the input/output variables which make it difficult to control a system efficiently. A minimal set of assumptions for existence of the decoupling controller formula is described in the state-space formulas. It is verified by an example.

• Aerospace Engineering and Technology
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• v.3 no.2
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• pp.160-169
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• 2004

In order to get the high resolution satellite image, MSC has TDI function in the KOMPSAT-2. So it is required to control the yaw angle of the attitude as operation concepts of KOMPSAT-2. This study was to explain the TDI function, to set up the geometric equation to satisfy the condition, and finally to determine the equation of yaw angle. The calculating program was developed and simulated with orbit and imaging attitude as input data, and the results were compared with the yaw steering values calculated in the on-board computer.