• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.44 no.12
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• pp.1043-1053
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• 2016

In this paper, the application of Parallel Distributed Compensation (PDC) controller for fixed pitch rotary wing system was studied. For nonlinear modeling, T-S fuzzy model was utilized to advance system control including the tilt type UAV. PDC controller was designed through the Linear Matrix Inequality (LMI). Experiments for determining the applicability and feasibility of PDC were performed using the 1 axis attitude control equipment and simulation. To verify the performance and characteristics of the controller, Mathworks Co. Simulink was used. After then, the PDC controller performance was verified and the results with developed controller using a 1 axis attitude control equipment were compared. Verification of the feasibility of PDC controller for the fixed pitch rotary wing system and identification of the overall performance and improvement analysis was conducted based on the experimental results.

• 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.

• Journal of the Korean Society for Marine Environment & Energy
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• v.17 no.3
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• pp.167-173
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• 2014

In this work, based on the blade element-momentum theory (BEMT), we proposed the geometry of a lab-scale horizontal axis tidal turbine with a diameter of 80cm, which can demonstrate the maximum power coefficient, and investigated the effect of blade pitch angle increase on the power coefficient. For validation of the computed power coefficients by the BEMT, we also computed the power coefficient using the computational fluid dynamics (CFD) for each case. For the CFD, 15 times of the turbine radius was used for the length and diameter of the computational domain, and the open boundary condition was prescribed at the boundary of the computational domain. The maximum power coefficients of the turbine acquired by the BEMT and CFD were about 48%, showing a good agreement. Both of the power coefficients computed by the BEMT and CFD tended to decrease when the blade pitch angle increases. The two power coefficients for a given tip-speed ratio were in good agreement. Through the present study, we have confirmed that we can trust the proposed geometry and the computed power coefficients based on the BEMT.

• Journal of the Korean Society for Precision Engineering
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• v.27 no.9
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• pp.26-33
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• 2010

A multi-MW wind turbine is a huge mechanical structure, of which the rotor diameter is more or less than 100 m. Rotor blades experience unsymmetric mechanical loads caused by the interaction of incoming wind with the tower and wind shear effect. These mechanical loads are transferred to the entire structure of the wind turbine and are known as the major reasons for shortening the life span of the wind turbine. Therefore, as the size of wind turbine gets bigger, the mitigation of mechanical loads becomes more important issue in wind turbine control system design. In this paper, a concept of an individual pitch control(IPC), which minimizes the mechanical loads of rotor blades, is introduced, and simulation results using IPC are discussed.

• Journal of the Korean Society for Precision Engineering
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• v.15 no.9
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• pp.33-42
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• 1998

If a ship diesel engine is operated by consolidated control with Controllable Pitch Propeller(CPP), the minimum fuel consumption is achieved together with the demanded ship speed. For this, it is necessary that the ship is operated on the ideal operating line which satisfies the minimum fuel consumption and that the pitch angle of CPP and throtle valve angle are controlled simultaneously. In this point of view, this paper presents a controller design method for a ship propulsion system with CPP based on the decoupling control theory. To do this, Linear Matrix Inequality(LMI) approach is introduced for the control system to satisfy the given $H_\infty$ control performance and robust stability in the presence of physical parameter perturbations. The validity and applicability of this approach are illustrated by simulation in the all operating ranges.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.11a
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• pp.72-77
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• 2008

The function of the Reaction Control System include roll, pitch and yaw control of the launch vehicles and fine control maneuvers and precision upper stage orientation before separation of one or more payload. This paper describes the overview of commercial launchers, current technology trend for RCS of launch vehicles, and development status of medium class thruster for RCS.

• Proceedings of the Acoustical Society of Korea Conference
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• 1995.06a
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• pp.119-122
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• 1995

음소단위의 포만트 합성방식을 이용하여 한국어의 규칙합성에 대해 시험하였다. 포만트 합성방식으로는 Klatt가 제안한 직/병렬 합성기를 수정하여 사용하였으며, 운율 정보를 나타내는 피치값의 제어는 Fujisaki 모델을 이용하였다. 합성에 사용되는 각 파라미터들이 합성음의 음질 및 파형에 미치는 영향을 분석할 수 있도록 합성 파라미터와 음성파형 및 스펙트로그램을 화면에 나타내고 마우스를 이용하여 파라미터 값을 사용자가 적절히 변경한 후 합성할 수 있는 포만트 방식의 합성 Tool을 개발하였으며, 이를 이용하여 한국어 문자/음성변환 시스템을 지속적으로 연구하고자 한다.

• Proceedings of the KIEE Conference
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• 2000.07b
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• pp.846-848
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• 2000

In the early development of wind energy, the majority of wind turbines were operated at constant speed. Recently, the number of variable-speed wind turbines adopted pitch control apparatus has increased. This paper deal with a simulation of pitch control of variable-speed wind turbine and the response of pitch angle is traced in a given random wind speed.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2012.05a
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• pp.136-136
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• 2012

최근 전자제품의 크기가 소형화, 고성능화 되어감에 따라 전자제품을 구성하는 부품 크기도 작아지고, 배선의 피치 또한 미세화 되고 있다. 따라서 패키징 과정도 미세하고 정확한 제어를 필요로 하게 되었으며, 전해도금을 통한 정밀 패키징 공정이 도입되고 있다. 그러나 기존에는 패키징용 메인기판과 부품을 연결하는 솔더는 기존의 Sn-Pb 조성의 납을 포함하는 소재가 사용되었다. 하지만 납의 환경적 문제에 의해 사용을 금지하게 된 상태로 이를 대체하기 위한 무연 조성의 솔더가 연구되고 있다.

• Proceedings of the Korean Institute of Intelligent Systems Conference
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• 2005.11a
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• pp.515-518
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• 2005

플립칩과 같은 정밀한 전자부품을 일반적인 표면실장방법에 의해 고속으로 장착 시킬 경우에는 칩의 표면이 PCB 실장면에 닿는 순간 접촉력(Contact Force)이 크게 발생한다. 과도한 접촉력에 의해 솔더 볼의 표면에 크랙이 가거나 솔더 볼이 변형되어 좁은 피치 내에서 인접해 있는 솔더 볼이 서로 붙는다든지, 또한 리드가 손상된다든지 하는 등과 같은 현상이 발생하여 표면 실장 불량의 원인이 될 가능성이 높아진다. 또한, 유연한 재질로 구성된 PCB 실장면에 과도한 힘을 가할 시에는 실장면의 국부적인 탄성변형이 발생하여 칩의 장착위치가 변경되어 정확한 위치에의 장착이 어렵게 된다. 따라서 CSP 나 플립 칩과 같은 고정도 칩을 고속으로 정확한 위치에 실장하기 위해서는 칩을 장착할 때 플립칩과 실장면의 자세를 평형상태로 제어할 필요가 있으며, 특히 발생하는 충격을 감소시키기 위한 충격 제어와 충돌 후 일정한 접촉력 유지를 할 수 있는 힘 제어가 필수적임을 알 수 있다. 따라서 본 논문에서는 상기와 같은 자세제어 및 힘제어를 요구하는 플립 칩 장착을 위한 엑츄에이터와 거리/힘 센서 시스템을 개발하였다. 제안된 시스템의 효율성을 입증하기 위해 다양한 환경에서 성능시험을 수행하였으며, 그 결과 제안된 시스템의 만족할 만한 실험결과를 보여주었다.