• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2007.12a
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• pp.307-308
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• 2007

In general, most physical systems are complex, highly non-linearity, affected by disturbance, incomplete knowledge, and even interactive change with the operating points. To solve this problem, the research of modem control theory and controller is proceeding. Before appling the proposed controller to the real system, however, it needs an apparatus which can verify the proposed controller for being not damaged the plant. In this paper, therefore, a RCGA-based PI-type state feedback controller using reduced-order observer is implemented and applied to the seesaw system and a series of simulation are carried out to verify the effectiveness of the control system.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.19 no.12
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• pp.2353-2363
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• 1994

This paper is concerned with the design of a robust digital controller using reduced-order observer on a robotic manipulator under the disturbance. In most cases of robotic manipulator since all state vectors are not measurable, the unmeasurable state vectors must be estimated or reconstructed. Other problems are caused by the nonlinear element like as nondifferentiable Coulomb friction, disturbance due to the gravitational pull, and the torsional spring effect of a link between the drive motor and the manipulator arm. The controller is based on feeding back the observable variables and the estimated state variables which are generated by the observer, and augmenting the system by additional discrete integrators. The feedback gain parameters are obtained by first applying the optimal control theory and then readjusting the feedback parameters to eliminate the limit cycle by using describing Function for nonlinear hybrid system.

• Journal of the Korean Institute of Navigation
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• v.2 no.1
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• pp.35-47
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• 1978

본 논문은 선박의 계산기제어문제의 일환으로서 일정한 속력으로 계로를 따라 항해하는 선박을 대상으로 조타계를 계산하는 문제를 취급한다. 설계의 지침으로써는 선박이 대양을 항해함에 있어서 예상되는 외란으로 인하여 증가되는 항로 및 외란의 영향을 제거하기 위해 취하는 조타운동으로 인한 속력의 손실을 항로의 연장 또는 항해시간의 연장이라는 고나점에서 2차형식의 평가함수를 선정하고, 이 평가함수를 최소로하는 의미에서 최적조타계를 설계한다. 실제로 최적조타계를 실현하기 위해서 적합관측기를 도입하였으며, 계산기의 시뮤레이션에 의해 본논문에서 제안한 최적조타계의 유효성을 입증하였다. 실선실험에 의해 조타운동과 속력감소의 관계를 확인하였으며, 위치오차로 인해 야기되는 문제점에 대해서도 약간의 고찰을 행하였다.

• Proceedings of the Korean Institute of Intelligent Systems Conference
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• 2004.04a
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• pp.502-505
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• 2004

An intelligent digital redesign technique (IDR) for the observer-based output feedback Takagi-Sugeno (T-S) fuzzy control system with unmeasurable premise variables is developed. The considered IDR condition is cubically parameterized as convex minimization problems of the norm distances between linear operators to be matched.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.47 no.4
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• pp.309-318
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• 2019

The thermal design of the Lunar Terrain Imager (LUTI) on the Korean Pathfinder Lunar Orbiter (KPLO) was performed and the soundness of the thermal design was verified by thermal analysis. The thermal environment of the lunar mission orbit should be reflected in the thermal design because the IR radiation of the lunar surface is important, unlike the earth orbit. The components or modules exposed to the outside of the satellite are insulated with MLI as much as possible, but the camera tube and the radiator are functionally exposed, so the thermal shield using the concept of radiation shape factor is mounted on the front to mitigate IR radiation. The IR emissivity is important in the front side of the radiator that receives little solar radiation, and components that are susceptible to thermal deformation such as the tube use a radiation heater to minimize the temperature gradient. Through the investigation of computational results, it was confirmed that the thermal design of LUTI is stable in various situations.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.38 no.3
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• pp.228-235
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• 2010

This paper deals with an autonomous flight controller design problem for a tilt-rotor aircraft in rotary-wing mode. The inner-loop algorithm is designed using the output-based approximate feedback linearization. The model error originated from the feedback linearization is cancelled within allowable tolerance by using single-hidden-layer neural network. According to Lyapunov direct stability theory, the adaptive update law is derived to run the neural network on-line, which is based on the linear observer dynamics. Moreover, the outer-loop algorithm is designed to track the trajectory generated from way-point guidance. Especially, heading and flight-path angle line-of-sight guidance are applied to the outer-loop to improve accuracy of the landing tracking performance. The 6-DOF nonlinear simulation shows that the overall performance of the flight control algorithm is satisfactory even though the collective input response shows instantaneous actuator saturation for a short time due to the lack of the neural network and the saturation protection logic in that loop.

• Journal of the Korean Institute of Intelligent Systems
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• v.25 no.1
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• pp.7-14
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• 2015

To implement an automatic picking system (APS) in distribution center with high precision and high dynamics, this paper presents a high gain observer-based robust speed controller design for a linear induction motor (LIM) drive. The force disturbance as well as the mechanical parameter variations such as the mass and friction coefficient gives a direct influence on the speed control performance of APS. To guarantee a robust control performance, the system uncertainty caused by the force disturbance and mechanical parameter variations is estimated through a high gain disturbance observer and compensated by a feedforward manner. While a time-varying disturbance due to the mass variation can not be effectively compensated by using the conventional disturbance observer, the proposed scheme shows a robust performance in the presence of such uncertainty. A Simulink library has been developed for the LIM model from the state equation. Through comparative simulations based on Matlab - Simulink, it is proved that the proposed scheme has a robust control nature and is most suitable for APS.

• Proceedings of the KIEE Conference
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• 2004.07d
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• pp.2245-2247
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• 2004

본 논문에서는 미지의 유계를 가진 불확실성을 포함한 비선형 시스템에 대한 고장 진단 설계를 제안한다. 제안된 고장 진단 필터는 비선형 관측기 설계 기술에 기초하여 설계되며, 신경망을 이용하여 고장 성분과 불확실성 성분을 추정하고 추정된 불확실성의 상한값을 고장 진단에 이용한다. 제안된 근사기는 불확실성과 고장 함수를 추정함으로써 고장 검출뿐만 아니라 고장 진단을 확인할 수 있도록 설계된다. 모의실험을 통해서 제안된 고장 진단 설계의 성능을 검증하였다.

• The Bulletin of The Korean Astronomical Society
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• v.36 no.2
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• pp.150.1-150.1
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• 2011

한국천문연구원은 미국 텍사스 대학 및 경희대와 함께 2개의 적외선 고분산 분광기 프로젝트를 진행하고 있다. 2013년 완성을 목표로 진행하고 있는 IGRINS ((the Immersion GRating INfrared Spectrograph) 는 최종 설계를 완료하여 지난 8월 25일 최종 설계 검토 회의를 진행하였으며, 내년 상반기까지 제작, 하반기 실험실 정렬을 거쳐 2013년맥도날드 2.7미터 부착 시험 관측을 예정하고 있다. 한국이 참여하고 있는 거대망원경 GMT (Giant Magellan Telescope)의 제 1세대 관측기 기로 제안한 고분산 적외선 분광기 GMTNIRS 는 IGRINS의 성능에 J, L, M band 분광기능을 더한 것이다. 총 6개의 개념 설계 기기중 하나로 선정되어 지난 1년간 개념설계를 진행해 왔으며, 10월 3일 최종 개념 설계 검토 회의를 진행할 예정이다. 이 두 기기의 성능, 현재까지의 진행상황 그리고 앞으로의 계획에 대해 설명한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.6
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• pp.431-441
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• 2020

In this paper, we propose a new method using a feedforward disturbance observer that guarantees stability and robustness about the effects of external disturbance and model uncertainty. The method is consist of a disturbance observer, a feedforward controller, and an overshoot detecting logic. It has an advantage of reducing the excessive overshoot by external disturbance and model uncertainty. Also, it is easy to adjust the control gain due to a simple structure. In order to verify the effectiveness of a new method, simulation results are given for longitudinal model of F-16 aircraft. By reflecting a various of model uncertainties, the stability and the robustness are guaranteed. Finally, the stability and the robustness of the proposed method are verified using root locus plot and bode plot.