• 한국지능시스템학회논문지
• /
• 제8권2호
• /
• pp.117-127
• /
• 1998

전력계통은 번개, 폭우, 고장등이 여러요인으로 인해 변화하는 동특성을 갖는다. 전송선로의 리액터스가 사고로 인해 변하는 것도 그 대표적인 예이며 전력게통에 불확성을 야기시키는 원인이 된다. 이경우, 이와같은 불확실성에 대해 견실한 성능을 발휘하는 제어기가 필요하다. 한편, 최근의 연구들을 통해 비파라미터적인 불확실서을 갖는 계통에 대해 퍼지제어기가 우수한 성능을 발휘함이 입증되었다. 따라서, 본 논문에서는 선로의 고장 발생시, 전력계통의 발전기 단자전압을 일정값으로 유지하며 계통을 안정화시킬 수 있는 적응퍼지제어기를 궤환선형화 기법에 근거하여 설계하고자 한다. 아울러 본 논문에서는 불확실한 계통에 있어서, 리아프노프 안정도를 보장 받기우해 필요한 불확실한 항의 상계를 퍼지계통에 으해 추정하는 방법을 제안한다. 시뮬레인션 결고, 설계된 제어기가 선로고장에도 불구하고 계통의 전압유지와 과도 안정도를 잘 보장해 줌을 확인할 수 있었다.

• Advances in aircraft and spacecraft science
• /
• 제5권3호
• /
• pp.335-348
• /
• 2018

The structural dynamics (SD) behavior of Elastic Flapping Wings (EFWs) is investigated analytically as a novel approach in EFWs analysis. In this regard an analytical SD solution of EFW undergoing a prescribed rigid body motion is initially derived, where the governing equations are expressed in modal space. The inertial forces are also analytically computed utilizing the actuator induced acceleration effects on the wing structure, while due to importance of analytical solution the linearity assumption is also considered. The formulated initial-value problem is solved analytically to study the EFW structural responses, where the effect of structure-actuator frequency ratio, structure-flapping frequency ratio as well as the structure damping ratio on the EFW pick amplitude is analyzed. A case study is also simulated in which the wing is modeled as an elastic beam with shell elements undergoing a prescribed sinusoidal motion. The corresponding EFW transient and steady response in on-off servo behavior is investigated. This study provides a conceptual understanding for the overall EFW SD behavior in the presence of inertial forces plus the servo dynamics effects. In addition to the substantial analytical results, the study paves a new mathematical way to better understanding the complex role of SD in dynamic EFWs behavior. Specifically, similar mathematical formulations can be carried out to investigate the effect of aerodynamics and/or gravity.

• International Journal of Advanced Culture Technology
• /
• 제11권2호
• /
• pp.10-29
• /
• 2023

Grit or perseverance as a factor for student success and life has gained increasing attention. Statistical methods have been the norm in analyzing various aspects of grit, but they do not address the transient and dynamic behavior well. We, for the first time, developed two linear dynamical models that specifically address the feedback structure of a child's desire to achieve a high grade point average (GPA) and the necessary effort that will increase stress between parents and a child. We call the dynamical model as GSES (Goal, Status, Effort & Stress). The two dynamical models incorporate the positive (i.e., achieving a high GPA) and the negative sides (i.e., effort and elevated stress and thus unhappiness) for being gritty or perseverant. Different types of parenting style and a child's characteristics were simulated whether parents and a child are empathetic or stubborn to their expectations and stress (i.e., willing or unwilling to change). Simulations show that when both parents and a child are empathetic to each other's expectation and stress, the most stable situations with minimal stress and effort occur. When a stubborn parent's and a stubborn child were studied together, this resulted in the highest elevation of stress and effort. Stubborn parents and a complying or empathetic child resulted in considerably high stress to a child. Interference from parents may unexpectedly result in a situation in which a child's stress is seriously elevated. The GSES model shows the U-shaped happiness curve (i.e., reciprocal of stress) caused by the increasing and then decreasing goal

• 드라이브 ㆍ 컨트롤
• /
• 제13권3호
• /
• pp.24-31
• /
• 2016

The performance characteristics of a dynamic control system are evaluated according to the transient and steady-state responses. The transient performance is the controllability of the output for the tracking of the reference or the ability to reduce or reject the effects of unwanted disturbances; alternatively, the steady-state performance is represented by the magnitude of the control error at the steady state. As the effects of the two performances on each other are reciprocal, a controller design that shows a zero steady-state error for the ramp input is uncommon because of the challenge regarding the achievement of an acceptable transient response. This paper proposes a PI+double-integral controller for the elimination of the steady-state error for the ramp input while a sound transient performance is maintained. The control-gain design procedure is described by the second-order response for the step input and the response of the error dynamics for the ramp input. The PI+double-integral controller is designed for the first-order transfer function that is derived from a system identification with the open-loop experiment data of the dc-motor. The simple structure of the proposed controller enables the adoption of a low-end microcontroller for the implementation of a real-time control. The experiment results show that the control performance is as effective as that of the simulation analysis for the operating point of linear system; furthermore, the PI+double-integral controller can be conveniently applied to the control system, which is desirable for the improvement of the steady-state error.

• 대한환경공학회지
• /
• 제38권1호
• /
• pp.25-33
• /
• 2016

본 연구에서는 수처리 공정에 적용하고 있는 CSTR 반응조를 대상으로 유입 유량이 다양하게 변동하는 경우 반응조 내부 수리 거동을 조사하고자 하였다. 유입 유량의 변동은 설계 유량 대비 10~100%까지 변화시켰으며, 각 경우를 CFD 기법을 이용하여 transient 상태의 추적자 실험을 모의하였으며, 모사 결과로부터 2차 정보를 추출하여 수리 거동 지표를 계산하여 유입 유량과 수리거동의 관계를 면밀히 조사하였다. 그 결과, 유입 유량이 증가할수록 Modal index와 ${\beta}$값이 증가하는 거동을 보였으며 Morrill index는 유입 유량과의 관계에서 국부적인 극소값을 가지는 유입 유량이 두 곳 나타났는데 각각 설계 유량의 20%되는 지점과 40%가 되는 지점이었다. 두 극소값이 나타나는 유입 유량보다 유량이 증가하면 다시 Morrill index가 증가하는 현상을 보여 이상적인 CSTR 반응조에 근접하는 것으로 나타났다.

• International Journal of Fluid Machinery and Systems
• /
• 제1권1호
• /
• pp.1-9
• /
• 2008

In the first part of the paper, Computational Fluid Dynamics analysis of the combusting flow within a high-swirl lean premixed gas turbine combustor and over the $1^{st}$ row nozzle guide vanes is presented. In this analysis, the focus of the investigation is the fluid dynamics at the combustor/turbine interface and its impact on the turbine. The predictions show the existence of a highly-rotating vortex core in the combustor, which is in strong interaction with the turbine nozzle guide vanes. This has been observed to be in agreement with the temperature indicated by thermal paint observations. The results suggest that swirling flow vortex core transition phenomena play a very important role in gas turbine combustors with modern lean-premixed dry low emissions technology. As the predictability of vortex core transition phenomena has not yet been investigated sufficiently, a fundamental validation study has been initiated, with the aim of validating the predictive capability of currently-available modelling procedures for turbulent swirling flows near the sub/supercritical vortex core transition. In the second part of the paper, results are presented which analyse such transitional turbulent swirling flows in two different laboratory water test rigs. It has been observed that turbulent swirling flows of interest are dominated by low-frequency transient motion of coherent structures, which cannot be adequately simulated within the framework of steady-state RANS turbulence modelling approaches. It has been found that useful results can be obtained only by modelling strategies which resolve the three-dimensional, transient motion of coherent structures, and do not assume a scalar turbulent viscosity at all scales. These models include RSM based URANS procedures as well as LES and DES approaches.

• 한국물환경학회지
• /
• 제30권2호
• /
• pp.166-174
• /
• 2014

Velocity gradient, G, a measure of the average velocity gradient in the fluid has been applied for complete mixing of chemicals in mechanical mixing devices. G values were calculated by the power input transferred to fluid in turbulent and transient range. Chemical reactions occur so fast that total mass transfer time required for even distribution of the chemicals determine the overall reaction time. The total mass transfer time is composed of the time for complete mixing through the reactor and for diffusion of the chemicals into the eddy. Complete mixing time was calculated by CFD (computer fluid dynamics) and evaluated by tracer tests in 2 liter jars at different rotating speeds. Turbulent range, Reynolds number above 10,000 in regular 2 liter jars occurred at revolution speed above 100 rpm (revolution per minute), while laminar range occurred at revolution speed below 10 rpm. A typical range of rotating speed used in jar tests for water and wastewater treatment was between 10 and 300 rpm, which covered both transient and turbulent range. G values supplied from a commercial jar test apparatus showed big difference from those calculated with power number specially in turbulent range. Diffusion time through eddy decreased 1.5 power-law of rotating speed. Complete mixing time determined by pumping number decreased increases in rotating speed. Total mass transfer time, finally, decreases as rotating speed increases, and it becomes 1 sec at rotating speed of 1,000 rpm. Complete mixing times evaluated from tracer tests showed higher than those calculated by power number at higher rotating speed. Complete mixing times, however, calculated by CFD showed similar to those of experimentally evaluated ones.

• Wind and Structures
• /
• 제22권2호
• /
• pp.211-234
• /
• 2016

Super long-span bridges provide people with great convenience, but they also bring traffic safety problems caused by strong wind owing to their high decks. In this paper, the large eddy simulation together with dynamic mesh technology in computational fluid dynamics (CFD) is used to explore the mechanism of a moving vehicle's transient aerodynamic force in crosswind, the regularity and mechanism of the vehicle's aerodynamic forces when it passes through a bridge tower's wake zone in crosswind. By comparing the calculated results and those from wind tunnel tests, the reliability of the methods used in the paper is verified on a moving vehicle's aerodynamic forces in a bridge tower's wake region. A vehicle's aerodynamic force coefficient decreases sharply when it enters into the wake region, and reaches its minimum on the leeward of the bridge tower where exists a backflow region. When a vehicle moves on the outermost lane on the windward direction and just passes through the backflow region, it will suffer from negative lateral aerodynamic force and yaw moment in the bridge tower's wake zone. And the vehicle's passing ruins the original vortex structure there, resulting in that the lateral wind on the right side of the bridge tower does not change its direction but directly impact on the vehicle's windward. So when the vehicle leaves from the backflow region, it will suffer stronger aerodynamic than that borne by the vehicle when it just enters into the region. Other cases of vehicle moving on different lane and different directions were also discussed thoroughly. The results show that the vehicle's pneumatic safety performance is evidently better than that of a vehicle on the outermost lane on the windward.

• 한국수자원학회논문집
• /
• 제57권4호
• /
• pp.263-276
• /
• 2024

지형구조가 복잡한 자연하천에서의 오염물질의 혼합과 이송 현상을 해석하기 위해 개발된 1차원 저장대 모형은 1970년대에 처음으로 제시된 이후 하천 내 오염물질의 정체 현상의 정확한 분석을 목적으로 다양한 형태로 개선되어 왔으며, 지난 수년간 지표수 및 지하수 분야에서 오염물질의 거동 및 체류시간을 예측하는 도구로써 활발히 활용되어 왔다. 그럼에도 불구하고 1차원 저장대 모형은 복잡한 자연하천의 혼합 기작을 제한된 매개변수를 통해 단순화하기 때문에 아직 해결되지 않은 숙제가 남아 있다. 본 리뷰 논문에서는 현재까지 개발된 저장대 모형의 장·단점을 설명하고, 모형의 구조적, 비구조적 불확실성에 대한 문제를 제기하고, 이를 극복하기 위해 필요한 연구의 방향성을 제시하였다. 본 연구 결과, 지속적인 정체시간분포 모델링에 대한 개선, 동수역학 해석 모형과 저장대 모형과의 결합, 그리고 추적자 실험 자료 수집 과정에서 불확도 개선을 통해 저장대 모형의 정확도를 향상시킬 수 있음을 알 수 있다. 모형의 복잡성을 증가시켜 정확도를 강화하는 방안은 지양하여야 하며, 모형 매개변수를 통한 하천의 정체특성 해석에는 수리·지형학적 근거와 추적자 실험 자료와 매개변수 추정 방식의 신뢰성이 함께 제시되어야 한다. 본 연구의 분석 결과와 제언은 저장대 모형을 통한 정밀한 하천 혼합 해석의 향후 연구에 토대가 될 것으로 기대한다.

• 생태와환경
• /
• 제37권3호통권108호
• /
• pp.304-312
• /
• 2004

수 생태계 내에서 흔히 볼 수 있는 3영양단계 먹이사슬 구조를 이루는 종들이 밀도비 의존 모델로써 구현 될 때 외부 환경에 대해서 어떻게 반응하는지를 연구하였다. 환경 요인은 주기적 요인과 일반적 노이즈 두 부분으로 나누었다. 주기적 요인이 온도로써 대표되었을 때 온도변이를 바이어스와 주기로 나누었고, 기타 복합적인 노이즈는 가우스 분포로 나타내었다. 온도변이 바이어스 ${\varepsilon}$, 온도주기 ${\Omega}$, 및 가우스 노이즈 크기 ${\'{O}}$가 서로 결합하여 3영양단계 먹이사슬에서 개체군 멸절을 포함한 다양한 개체군 동태를 보여 주었다. 변수의 적절한 값에 따라 '안정된 제한 사이클'이나 '이상한 끌개'를 보여 주었으며, 전체적으로 개체군 동태는 환경 변수에 따라 민감하게 반응하였고, 포식자 및 최상위포식자 개체군의 멸절시간이 조절되었다.