• 한국광학회:학술대회논문집
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• 한국광학회 2009년도 동계학술발표회 논문집
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• pp.305-306
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• 2009

This paper shows through detailed simulations that the length of conventionally designed multimode-interference couplers can be shorted significantly by stepped-width and stepped-index design. For the cross-coupling device, this stepped-design results in 9% or more length reduction.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2005년도 창립60주년 기념 추계 학술대회
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• pp.183.2-183.2
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• 2005

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2013년도 춘계학술대회 논문집
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• pp.823-824
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• 2013

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1989년도 한국자동제어학술회의논문집; Seoul, Korea; 27-28 Oct. 1989
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• pp.87-92
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• 1989

An autopilot for the class of Bank-To-Turn missiles is developed using a multivariable plant model & control design methodology. The roll-pitch-yaw cross coupling is included in the design considerations. Feedback system is designed using the Linear Quadratic Gaussian with Loop Transfer Recovery (LQG/LTR). Nonlinear simulations are presented to demonstrate the performances of the designed system.

• 대한화학회지
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• 제61권5호
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• pp.286-290
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• 2017

• 대한화학회지
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• 제61권5호
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• pp.296-298
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• 2017

• Bulletin of the Korean Chemical Society
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• 제31권1호
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• pp.250-252
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• 2010

• 응용통계연구
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• 제28권5호
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• pp.871-883
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• 2015

벡터자기회귀모형은 다차원의 시계열 자료간의 선형종속 관계를 연구하는데 효율적인 모형이다. 하지만 차원이 높아질 경우 추정해야할 모수가 급격히 증가하여 추정이 불안정해지고 예측력의 저하 및 해석의 어려움을 동반하는 문제를 가지고 있다. 이를 보완하기 위해서 많은 계수를 0으로 두는 희박벡터자기회귀모형이 제안되었고 고차원 시계열 분석에서 유용함이 밝혀졌다. 이 논문에서는 희박벡터자기회귀모형 추정에 있어서 어떠한 계수를 0으로 두어야 하는지를 판단해주는 한 쌍의 변수에 대한 상관 정도를 추정해주는 커플링 측도를 제안한다. 먼저 이 논문에서는 부분 스펙트럼 일관성에 기반을 둔 커플링 측도를 사용한 변수 선택의 경우 다른 변수의 효과를 제거한 잔차에 기반을 두었기에 좋은 효율성을 보임을 밝힌다. 하지만 부분 스펙트럼 일관성의 경우 벡터자기회귀모형 계수의 비대칭성을 고려하지 못한다는 단점이 있어 이를 보완하고자 필터링을 통해 다른 변수의 효과를 제거한 잔차에 기반을 둔 동시에 비대칭성을 가지는 커플링 측도들, 필터링된 잔차를 이용한 교차 상관성과 그래인저 인과관계를 제안한다. 모의실험을 통해 우리가 제안한 방법론들이 두터운 꼬리를 가지거나 높은 차수의 희박벡터자기회귀모형의 경우에도 매우 정확하게 0이 아닌 변수를 선택함을 보인다.

• Wind and Structures
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• 제34권5호
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• pp.437-450
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• 2022

Vortex-induced vibration (VIV) is a significant concern when designing slender structures with square cross sections. VIV strongly depends on structural dynamics and flow states, which depend on the conditions of the approaching flow and shape of a structure. Therefore, the effects of the angle of attack on the coupling effects of VIV for a square cylinder are expected to be significant in practice. In this study, the aerodynamic forces for a fixed and elastically mounted square cylinder were measured using wind pressure tests. Aerodynamic forces on the stationary cylinder are firstly discussed by comparisons of variation of statistical aerodynamic force and wind pressure coefficient with wind angle of attack. The coupling effect between the aerodynamic forces and the motion of the oscillating square cylinder by VIV is subsequently investigated in detail at typical wind angels of attack with occurrence of three typical flow regimes, i.e., leading-edge separation, separation bubble (reattachment), and attached flow. The coupling effect are illustrated by discussing the onset of VIV, characteristics of aerodynamic forces during VIV, and interaction between motion and aerodynamic forces. The results demonstrate that flow states can be classified based on final separation points or the occurrence of reattachment. These states significantly influence coupling effects of the oscillating cylinder. Vibration enhances vortex shedding, which creates strong fluctuations in aerodynamic forces. However, differences in the lock-in range, aerodynamic force, and interaction process for angles of attack smaller and larger than the critical angle of attack revealed noteworthy characteristics in the VIV of a square cylinder.

• 제어로봇시스템학회논문지
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• 제14권10호
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• pp.991-997
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• 2008

A new RMRAC scheme far the PMSM current regulation is proposed in a synchronous frame, which is completely free from the parameter's uncertainty. A current regulator of PMSM is the inner most loop of electromechanical driving systems and plays a foundation role in the control hierarchy. When the PMSM runs in high speed, the cross-coupling terms must be compensated precisely for large system BW. In the proposed RMRAC, the input signal is composed of a calculated voltage defined by MRAC law and an output of the disturbance compensator. The gains of feed forward and feedback controller are estimated by the proposed modified gradient method, where the system disturbances are assumed as filtered current regulation errors. After the compensation of the system disturbance from error information, the corresponding voltage is fed forward to control input to compensate for real disturbances. The proposed method robustly compensates the system disturbance and cross-coupling terms. It also shows a good realtime performance due to the simplicity of control structure. Through real experiments, the efficiency of the proposed method is verified.