• The Journal of Korean Institute of Communications and Information Sciences
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• v.28 no.11C
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• pp.1062-1069
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• 2003

This paper presents a new loop shaping technique for design of robust optimal PID controllers in order to satisfy the performance requirements. PID controller can be designed by selecting the suitable weighting factors Q and R. This technique is developed by pushing all two zeros formed by PID controller closely to a larger pole of the second order plant. As a result, a good loop shaping is achieved in the high frequencies region on the Bode plot. For the robust optimal tuning of PID controller for second order system, a new loop shaping procedure is developed via LQR approach.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2000.11a
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• pp.35-35
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• 2000

추력 편향제어(Thrust Vector Control)는 위성 발사체나 대륙간 탄도 미사일과 같이 공기가 희박한 고 고도에서의 비행자세 제어와 궤도수정, 지대공이나 함대공 유도탄처럼 발사 직후 저속에서 임의의 방향으로 급선회해야 할 경우에 노즐의 배출가스 방향을 직접 조절하여 모멘트를 발생시키는 제어방식을 말한다. 이 방식 중 널리 사용되고 있는 제트 베인 추력 편향제어방식은 베인이 직접 고온, 고속의 가스 흐름내에서 작용하기 때문에 재료는 내열성과 제트 베인 주위에 형성되는 유동 특성, 그리고 베인간의 유동 간섭이 중요한 인자이다. 그러므로, 제트 베인의 실용화는 수치해석에 의존하던 개발 초기나 중기의 설계 단계에서 벗어나 실제 크기나 축소모델의 유동 모사 시험에 의해 성능이 검증되어야 한다.(중략)

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.46 no.1
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• pp.10-17
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• 2018

The size of commercial wind turbines has been increased. Generally, the pitch control is used to increase the efficiency of wind turbine. However, the pitch control has difficulty to control the local unsteady flow control which makes fatigue load and decreases the efficiency. In this research, Synthetic Jet Actuators(SJAs) are manufactured and applied into a wing section to delay flow separation and increase aerodynamic performances. The SJAs as a kind of zero-net mass-flux actuators injects and removes fluid through a small orifice with a given frequency. The SJA modules actuated by piezoelectric disks are manufactured and the aerodynamic performances are measured according to the shape of the orifice and the velocity of the jets through the wind tunnel test. It is confirmed that as the velocity of the jets are increased using rectangular shape orifice, drag force is decreased and lift force in increased.

• Journal of the Korean Society of Marine Environment & Safety
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• v.21 no.2
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• pp.200-206
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• 2015

In order to verify the lift enhancement of the 2D hydrofoil with trailing edge rotor and check the ability of its practical use, experimental studies were conducted in the caviation tunnel using the test model with NACA0020 section. The three-component forces acting on the model could be measured by exclusively designed sting type multi-component load cell. The trailing edge of the model has been replaced with rotor which could be controlled by DC servo motor installed at the exterior of the tunnel. A typical effect of the trailing edge rotor has been introduced among the systematic experiments on various angular deviation of the model and the rotational velocity of the trailing edge rotor. It is appeared that the circulation control effect could be easily adjusted by selecting the rotational velocity of the trailing edge rotor and the lift force was augmented more than two times. Thus the proposed lifting device could be utilized as a novel high lifting device which has adjustability of lift force.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.6
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• pp.59-66
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• 2006

Acoustic cavity as a stabilization device to control high-frequency combustion instabilities in liquid rocket engine is adopted and its damping capacity is verified in atmospheric temperature. First, harmful resonant frequency in a modeling chamber can be damped effectively by the installation of properly-tuned acoustic cavity. Besides, geometric effects of acoustic cavity on damping characteristics are analyzed and compared quantitatively. Satisfactory agreements have been achieved with linear acoustic analysis and experimental approach. Results show that the acoustic cavity of the largest orifice area or the shortest orifice length was the most effective in acoustic damping of the harmful resonant frequency. Finally, it is proved that an optimal design process is indispensable for the effective control of combustion instabilities.

• Proceedings of the Korea Water Resources Association Conference
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• 2010.05a
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• pp.1971-1975
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• 2010

하천은 자연의 현상 또는 인위적인 작용에 대해 끊임없는 반응과 응답의 과정을 통하여 복잡한 형태의 안정화를 이루고 있다. 하지만 인간은 경제적인 논리와 편의성 측면등의 이유로 하천에 대해 인위적인 간섭이 지속적으로 이루어져 왔다. 이는 하천이 본래 가지고 있던 자연적인 하도 특성의 급격한 변화를 초래하였다. 이러한 영향으로 인한 많은 변화들 중, 하도 내 수역이 식생으로 천이가 진행되면서 최종적으로 육지화되는 육역화 현상은 수리학적 문제 및 환경생태적 측면에서 큰 문제를 발생시킬 수 있다. 따라서 본 연구에서는 하도육역화를 제어하기 위해 하도 내 친환경적인 육역화 관리기법을 개발하고 이에 대한 적용성을 수리모형실험을 통해 제시하고자 한다. 이를 위해 본 연구에서 제시한 친환경적인 육역화 관리기법은 자연적인 배수효과를 이용 하였다. 이러한 친환경적인 육역화관리기법은 인공하도가 가지고 있는 하도와 고수부지의 수문학적 및 생태학적인 단절을 해소하였으며, 이를 물골 공법이라 명명하였다. 본 수리모형실험은 물골의 형상을 제시하기 위하여 하폭에 따라 물골크기를 무차원화 하였다. 또한 유사 제어 검증을 수행하기 위한 실험은 물골의 폭, 높이, 주기 및 가속수로 폭을 실험변수로 고려하였다. 물골 모형의 기본적인 흐름특성 분석을 위해 유속 및 수위를 측정한 결과 유속 및 수심은 하류를 따라 증가하는 경향을 보였다. 또한 유사 제어 효과 검증을 위해 소류력 및 마찰속도를 산정하여 도시하였으며, 이는 세굴 및 퇴적의 현상이 물골 주기에 따라 반복적으로 나타났다. 이러한 결과는 수위하강시 물골의 형상에 따라 흐름이 원활하게 배제되어 고수부지에 유사퇴적 방지 효과가 있을 것으로 판단되며, 물골공법이 친환적인 육역화 관리기법으로 활용가능성이 있는 것으로 기대된다. 향후 보다 상세한 수리모형실험이 수행된다면, 물골 공법 설계 및 현장적용을 위한 기초자료를 확보 할 수 있을 것이다.

• Composites Research
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• v.32 no.5
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• pp.265-269
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• 2019

The direct spinning of carbon nanotube (CNT) fibers is a promising method in the high performance composite materials. However, most of the reported CNT arrays do not have spinning properties because of their limited synthesis conditions. In this study, we investigate the properties of spinnable CNT arrays, which is closely related to the morphology of CNT array. The array morphology controlled by controlling the conditions of catalyst, carbon source, etc. By additional carbon source of ethylene and changing the composition of the catalyst, the waviness of the CNT array can be remarkably reduced, which leads to improve of the spinning properties. The synthesized CNT arrays were well aligned along c-axis and the synthesis conditions of the spinning array could be derived.

• Journal of Korean Association for Spatial Structures
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• v.7 no.3 s.25
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• pp.57-66
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• 2007

The membrane structures, a kind of lightweight soft structural system, are used for spatial structures. The material property of the membrane has strong axial stiffness, but little bending stiffness. The design procedure of membrane structures are needed to do shape finding, stress-deformation analysis and cutting pattern generation. In shape finding, membrane structures are unstable structures initially. These soft structures need to be introduced initial stresses because of its initial unstable state, and happen large deformation phenomenon. Therefore, in this paper, we investigate the convergence of solution and the speed according to the control variables and the method of shape analysis.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.25 no.1
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• pp.101-108
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• 2012

Initial shape analysis for cable-stayed bridges should be able to find optimizated initial cable forces and unstrained length that minimize deflection and bending moments of the deck and pylon. Comparison study of an improved initial force method and TCUD method for determination of initial cable forces in cable-stayed bridges is presented in this paper. For this purpose, an elastic catenary cable element and a nonlinear frame element are firstly described. And concepts and algorithm of two analysis methods are then presented. Finally to demonstrate the validity and the accuracy of two methods, numerical examples for initial state problems of cable-stayed bridges are given and compared based on these methods.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2007.11a
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• pp.199-200
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• 2007