• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2003.05a
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• pp.72-75
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• 2003

In this research, we focused on the effects of the orifice internal flow such as cavitation and hydraulic flip. The breakup characteristics such as the breakup length and trajectory were measured by changing the orifice diameter (d), the orifice length/orifice diameter (L/d), the injection pressure and the shapes (sharp and round) of orifice entrance to provide a lot of conditions of the orifice internal flow. It is found that cavitation bubbles that occur inside the sharp-edged orifice make the liquid jet ejecting from the orifice turbulent. In the orifices (L/d = 5), the hydraulic flip phenomenon is shown when the injection pressure is high. In case cavitation occurs it breaks up more earlier than that in case of non-cavitation. In case hydraulic flip occurs, since the area of the liquid jet becomes small, the breakup length is also small as that in case of cavitation. But the liquid column trajectories have a similar tendency irrespective of cavitation.

• Aerospace Engineering and Technology
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• v.13 no.2
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• pp.18-28
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• 2014

We assume that two control moment gyros are installed for space qualification in a satellite with four reaction wheels, and study the high agile maneuver method. Using high torque control moment gyros, we reduce the satellite's attitude error. After that, we activate reaction wheels to control remaining attitude error. This proposed method can avoid singularity problem of control moment gyros, and do not require gimbals' angle to calculate torque command. Through numerical simulations, we show that our method's agile performance is similar to previous method and reduce the reaction wheels' required momentum.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.21 no.3
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• pp.392-404
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• 1997

The flow induced by the oscillatory motion of a solid body is important in a number of practical problems. As the solid boundary oscillates harmonically, there is steady streaming motion invoked by the Reynolds stresses, which could cause extensive migration of the fluid during a period of fluid motion. We here analyzed the flow in a square cavity with an oscillating top wall for the parameters which make the time derivatives and the convective terms equally important in the entire cavity flow. The full Navier-Stokes equations are solved by the second-order time accurate Momentum Coupling Method which is devised by the authors. The particular numerical scheme does not need subiteration at each time step which is usually a required process to calculate the incompressible Navier-Stokes equations. The effect of two parameters, the Reynolds number and the frequency parameter, on the oscillatory flow has been investigated.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.4
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• pp.70-76
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• 2002

Characteristics of kerosine spray combustion were investigated at various swirl condition. PDPA(Phase Doppler Particle Analysis) was used to measure the droplet sizes and velocities. R-type(Platinum vs. Platinum-13%rhodium) thermocouple was used to measure the temperature of combustion flow field inside model combustor. A visualization of spray and flame was performed with still camera. As swirl number increases due to increase of swirl vane angle, the spray and the flame were developed to radial direction rapidly. When swirl number is small, the configuration of flame is cone type, but swirl number is large, the configuration of flame is cylindrical type due to enhanced mixing by the transport of swirl momentum.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.7
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• pp.648-656
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• 2015

Active SAR satellite's main maneuver is roll axis maneuver to change SAR antenna direction. In addition, yaw steering is required to minimize the doppler centroid variation. Thus, it is resonable to assign the torque/momentum capacity mostly to roll axis and then yaw axis. In this case, the pitch axis shows low agility performance. However, due to orbit maintenance, large angle maneuver about pitch axis is sometimes required. In this paper, we study the pitch axis maneuver time reduction through sequential rotation about roll and yaw axis. Since these two axes have high agility performance than pitch axis, maneuver time reduction is possible when large angle rotation about pitch axis is required.

• Proceedings of the Korea Water Resources Association Conference
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• 2005.05b
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• pp.904-907
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• 2005

본 연구에서는 강우량의 실측치인 자동기상관측소(AWS) 자료와 현재의 대기상태인 인공위성(GMS-5호) 자료를 입력자료로 하여 현재부터 3시간 선행시간까지의 면적평균강우량을 예측할 수 있도록 강우예측 신경망 모형을 개발하였으며, 2002년 8월 집중호우시 남강댐 유역에 적용하였다. 신경망 모형의 학습을 위해서 $1998\~2001$년 $6\~9$월과 2002년 6, 7월의 강우사상과 적외선 자료가 사용되었고, 학습이 종료되면 예측기간(2002년 8월 $6\~16$일)동안의 강우예측이 수행되었다. 신경망 모형의 학습단계에서는 자료들간의 비선형 상관관계를 나타내는데 적합한 역전파 알고리즘 학습방법 중 모멘텀법을 사용하였으며, 신경망 모형의 출력값은 현재부터 3시간 후까지의 면적평균강우량을 예측할 수 있도록 구성하였다. 예측된 면적평균강우량은 실제 관측된 강우량의 패턴은 잘 따르고 있었지만 첨두치를 과소평가하는 경향이 나타났다. 본 연구에서 개발된 신경망 모형은 관측된 강우자료의 품질과 패턴이 모형의 정확성에 미치는 영향이 절대적인 기존의 신경망 모형과 차별화하여, 현재의 대기상태를 나타내는 인공위성 자료를 추가함으로써 보다 정확한 강우량 예측이 가능하도록 하였다.

• Proceedings of the Korea Water Resources Association Conference
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• 2009.05a
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• pp.314-318
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• 2009

본 연구의 목적은 강우-유출자료 및 댐 방류량 자료의 비선형적인 특정을 가장 잘 반영할 수 있는 신경망모형을 적용하여 수질정책의 기초자료를 제공하기 위하여 신뢰성 있는 유량자료를 산정하는 모형을 개발하였고 이를 낙동강 유역에 적용하는 것이다. 이를 위해서 낙동강물환경연구소의 8일 측정 유량이 가지는 정확성을 이용하면서 상류 댐의 일 방류량자료와 유역별 강우자료 및 국토해양부 수위관측소의 수위자료를 연계하여 유량을 보간할 수 있는 유량 보간 신경망 모형을 개발하였다. 신경망 모형의 출력값은 낙동강물환경 연구소에서 측정하지 않은 기간에 대하여 유량을 보간할 수 있도록 구성하였으며 신경망 모형의 구조는 입력층과 출력층 사이에 하나의 은닉층이 존재하는 다층 신경망으로 구성하였으며, 학습단계에서는 오류 역전파 알고리듬 학습방법 중 모멘텀법을 사용하였다. 본 연구를 통하여 낙동강 전 유역에 대하여 유량 보간 모형을 적용한 결과 댐 방류량과 강우자료 및 상류 수위 관측소의 유량 자료를 이용한 유량 보간 신경망모형의 일 유량결과의 적용가능성을 검증할 수 있으며, 제시된 모형은 지속적인 수문자료의 질적 향상과 유출패턴의 축적으로 그 성능을 향상시킬 수 있을 것이며 또한 홍수기의 더 정확한 유량예측을 위한 적용사례의 확장 및 SWAT을 이용한 모형의 적용에 대한 연구가 병행되어야 할 것이다.

• Bulletin of the Korean Space Science Society
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• 2006.04a
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• pp.121-124
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• 2006

B-dot logic is generally used for controlling the initial tip-off rate. However, it has the disadvantage of taking a relatively long time to control the initial tip-off rate. To solve this problem, this paper suggests a new detumbling control method to be able to adapt to micro/nanosatellite with the pitch bias momentum system. Proposed detumbling method was able to control the angular rate within 20 minutes which is a significant reduction compared to conventional methods.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.7
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• pp.40-50
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• 2005

In this paper, preliminary results for performance prediction of a dual-rotor wind turbine generator system are presented. Blade element and momentum theories are used to model the aerodynamic forces and moments acting on the rotor blades, and multi-body dynamics approach is used to integrate the major components to represent the overall system. Not only the steady-state performance but the transient response characteristics are analyzed. Pitch control strategy to control the rotor speed and the generator output is proposed and its performance is verified through the nonlinear simulation.

• Journal of Intelligence and Information Systems
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• v.22 no.2
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• pp.115-125
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• 2016

The Bollinger Band indicating the current price position in the recent price action range is obtained by adding/substracting the simple standard deviation (SSD) to/from the simple moving average (SMA). In this paper, we first compare the characteristics of the SMA and the exponential moving average (EMA) in the operator's point of view. A basic equation is obtained between the interval length N of the SMA operator and the weighting factor ${\rho}$ of the EMA operator, that makes the centers of the 1st order momentums of each operator impulse respoinse identical. For equivalent N and ${\rho}$, frequency response examples are obtained and compared by using the discrete time Fourier transform. Based on observation that the SMA operator reacts more excessively than the EMA operator, we propose a novel exponential standard deviation (ESD) band centered at the EMA and derive an auto recursive formula for the proposed ESD band. Practical examples for the ESD band show that it has a smoother bound on the price action range than the Bollinger Band. Comparisons are also made for the gap corrected chart to show the advantageous feature of the ESD band even in the case of gap occurrence. Trading techniques developed for the Bollinger Band can be straight forwardly applied to those for the ESD band.