• 제목/요약/키워드: Line-grid method

검색결과 249건 처리시간 0.027초

A novel PLL control method for robust three-phase thyristor converter under sag and notch conditions

  • Lee, Changhee;Yoo, Hyoyol
    • 전력전자학회:학술대회논문집
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    • 전력전자학회 2014년도 추계학술대회 논문집
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    • pp.87-88
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    • 2014
  • The paper presents a novel phase locked loop(PLL) control method for robust three-phase thyristor dual converters under sag, notch, and phase loss conditions. This method is applied to three line to line voltages of grid to derive three phase angle errors from three separated single-phase PLLs. They can substitute for abnormal phase to guarantee the synchronization in the various grid fault conditions. The performance of novel PLL with moving average method is verified through simulations.

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그리드지도의 방향정보를 이용한 형상지도 작성 (Feature based Map Building by using Orientation Information in a Grid Map)

  • 강승균;임종환
    • 한국정밀공학회지
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    • 제22권12호
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    • pp.61-69
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    • 2005
  • This paper presents an efficient method of extracting line segments from the occupancy grids in a grid map. The grid map is composed of 2-D grids that have both the occupancy and orientation probabilities using sonar sensors. We evaluate the orientation information of every grid when the occupancy probability of the grid is updated from sonar range data. To find the shape of an object in the map from orientation information, the orientations are clustered into several groups according to their values. The line segments are, then, extracted from the clusters based on Hough transform. Finally, a feature-based map is built with these line segments. The proposed method is illustrated with the results produced by sets of experiments in an indoor environment.

보존적 중첩격자기법을 이용한 동적 플랩의 천이적 공력거동에 관한 수치적 연구 (Numerical Study on Transient Aerodynamics of Moving Flap Using Conservative Chimera Grid Method)

  • 최성욱;장근식;김인선
    • 한국전산유체공학회지
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    • 제5권2호
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    • pp.9-19
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    • 2000
  • Transient aerodynamic response of an airfoil to a moving plane-flap is numerically investigated using the two-dimensional Euler equations with conservative Chimera grid method. A body moving relative to a stationary grid is treated by an overset grid bounded by a 'Dynamic Domain Dividing Line' which has an advantage for constructing a well-defined hole-cutting boundary. A conservative Chimera grid method with the dynamic domain-dividing line technique is applied and validated by solving the flowfield around a circular cylinder moving supersonic speed. The unsteady and transient characteristics of the flow solver are also examined by computations of an oscillating airfoil and a ramp pitching airfoil respectively. The transient aerodynamic behavior of an airfoil with a moving plane-flap is analyzed for various flow conditions such as deflecting rate of flap and free stream Mach number.

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Soroban grid 기반 CIP법을 이용한 자유표면 유동해석 (FREE SURFACE FLOW ANALYSIS BY SOROBAN GRID BASED CIP MEHTOD)

  • 임효남
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2010년 춘계학술대회논문집
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    • pp.326-334
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    • 2010
  • In this study, we provide a comprehensive review of the CIP(Constrained Interpolation Pro file/Cubic Interpolated Propagation) method with a pressure-based algorithm that is known as a general numerical solver for soled liquid, gas and plasmas. And also we introduce a body-fitted grid system(Soroban grid) for computation of strongly nonlinear marine hydrodynamic problems such as slamming water on deck, wave impact by green water. This grid system can keep the third-order accuracy in time and space with the help of the CIP method. The grid system consists of the straight lines and grid points. In the 2-dimensional grid case, each grid points moving in these lines like abacus - Soroban in Japanese. The length of each line can be different and the number of grid points in each line can be different. Mesh generation and searching of upstream departure point are very simple and possible to mesh-free treatment. To optimize computation of free-surface and multi-fluid flows, We adopt the C-CUP method. In most of the earlier computations, the C-CUP method was used with a staggered-grid approach. Here, because of the mesh free nature of the Soroban grid, we use the C-CUP method with a collocated-grid approach.

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An Optimization Method for the Calculation of SCADA Main Grid's Theoretical Line Loss Based on DBSCAN

  • Cao, Hongyi;Ren, Qiaomu;Zou, Xiuguo;Zhang, Shuaitang;Qian, Yan
    • Journal of Information Processing Systems
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    • 제15권5호
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    • pp.1156-1170
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    • 2019
  • In recent years, the problem of data drifted of the smart grid due to manual operation has been widely studied by researchers in the related domain areas. It has become an important research topic to effectively and reliably find the reasonable data needed in the Supervisory Control and Data Acquisition (SCADA) system has become an important research topic. This paper analyzes the data composition of the smart grid, and explains the power model in two smart grid applications, followed by an analysis on the application of each parameter in density-based spatial clustering of applications with noise (DBSCAN) algorithm. Then a comparison is carried out for the processing effects of the boxplot method, probability weight analysis method and DBSCAN clustering algorithm on the big data driven power grid. According to the comparison results, the performance of the DBSCAN algorithm outperforming other methods in processing effect. The experimental verification shows that the DBSCAN clustering algorithm can effectively screen the power grid data, thereby significantly improving the accuracy and reliability of the calculation result of the main grid's theoretical line loss.

Design and Control Method for Sub-module DC Voltage Ripple of HVDC-MMC

  • Gwon, Jin-Su;Park, Jung-Woo;Kang, Dea-Wook;Kim, Sungshin
    • Journal of Electrical Engineering and Technology
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    • 제11권4호
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    • pp.921-930
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    • 2016
  • This paper proposes a design and control method for a high-voltage direction current modular multilevel converter (HVDC-MMC) considering the capacitor voltage ripple of the submodule (SM). The capacitor voltage ripple consists of the line frequency and double-line-frequency components. The double line- frequency component does not fluctuate according to the active power, whereas the line-frequency component is highly influenced by the grid-side voltage and current. If the grid voltage drops, a conventional converter increases the current to maintain the active power. A grid voltage drops, current increment, or both occur with a capacitor voltage ripple higher than the limit value. In order to reliably control an MMC within a limit value, the SM capacitor should be designed on the basis of the capacitor voltage ripple. In this paper, the capacitor voltage ripple according to the grid voltage and current are analyzed, and the proposed control method includes a current limitation method considering the capacitor voltage ripple. The proposed design and control method are verified through simulation using PSCAD/EMTDC.

다른 선폭들로 구성된 격자형 교정판을 이용한 간단한 카메라 교정 시스템의 개발 (A development of the simple camera calibration system using the grid type frame with different line widths)

  • 정준익;최성구;노도환
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1997년도 한국자동제어학술회의논문집; 한국전력공사 서울연수원; 17-18 Oct. 1997
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    • pp.371-374
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    • 1997
  • Recently, the development of computer achieves a system which is similar to the mechanics of human visual system. The 3-dimensional measurement using monocular vision system must be achieved a camera calibration. So far, the camera calibration technique required reference target in a scene. But, these methods are inefficient because they have many calculation procedures and difficulties in analysis. Therefore, this paper proposes a native method that without reference target in a scene. We use the grid type frame with different line widths. This method uses vanishing point concept that possess a rotation parameter of the camera and perspective ration that perspect each line widths into a image. We confirmed accuracy of calibration parameter estimation through experiment on the algorithm with a grid paper with different line widths.

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하이브리드 방법을 이용한 격자 패턴의 세그먼테이션 (The Grid Pattern Segmentation Using Hybrid Method)

  • 이경우;조성종;주기세
    • 한국정보통신학회논문지
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    • 제8권1호
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    • pp.179-184
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    • 2004
  • 본 논문은 하이브리드 방법을 사용하여 영상내의 체형 외곽 선과 격자 패턴을 추출하여 3차원 체형 데이터를 획득하기 위한 새로운 영상분할 알고리즘을 제안한다. 체형 외곽 선을 추출하기 위한 영상분할 방법으로 최대 값 인식 알고리즘을 사용하였다. 이 방법은 에지에서의 접선 방향 값은 작지만 법선 방향 값은 큰 성질을 이용하여 일정 영역내의 픽셀들간의 변화 값 중 최대 값을 인식하는 알고리즘이다. 그리고 체형 외곽내의 격자 패턴은 격자 패턴 검출 알고리즘을 사용하여 추출하였다. 추출된 체형 외곽 선과 격자 패턴을 결합한 후 휴리스틱 방법인 연속 길이 테스트에 치한 격자 패턴의 연결 및 잡음제거를 하였다. 본 논문에서 제안한 영상분할 방법은 기존의 기울기나 라플라시안 연산방법보다 매우 효과적인 결과를 가져 왔다.

그리드지도의 방향정보 이용한 형상지도형성 (Feature Map Construction using Orientation Information in a Grid Map)

  • 송도성;강승균;임종환
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2004년도 추계학술대회 논문집
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    • pp.1496-1499
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    • 2004
  • The paper persents an efficient method of extracting line segment in a grid map. The grid map is composed of 2-D grids that have both the occupancy and orientation probabilities based on the simplified Bayesian updating model. The probabilities and orientations of cells in the grid map are continuously updated while the robot explorers to their values. The line segments are, then, extracted from the clusters using Hough transform methods. The eng points of a line segment are evaluated from the cells in each cluster, which is simple and efficient comparing to existing methods. The proposed methods are illustrated by sets of experiments in an indoor environment.

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보존적 중첩격자기법을 이용한 동적 플랩의 천이적 공력거동에 관한 수치적 연구 (Numerical Study on Transient Aerodynamics of Moving Flap Using Conservative Chimera Grid Method)

  • 최성욱;장근식
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 1999년도 추계 학술대회논문집
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    • pp.85-94
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    • 1999
  • Transient aerodynamic response of an airfoil to a moving plane-flap is numerically investigated using two-dimensional Euler equations with conservative Chimera grid method. A body moving relative to a stationary grid is treated by an overset grid bounded by a 'dynamic domain-dividing line' the concept of which is developed in this study. A conservative Chimera grid method with a dynamic domain-dividing line technique is applied and validated by solving the flowfield around circular cylinder moving supersonic speed. The unsteady and transient characteristics of the flow solver is also examined by computations of a oscillating airfoil and a ramp pitching airfoil respectively. The transient aerodynamic behavior of an airfoil with a moving plane-flap is analyzed for various flow conditions such as deflecting rate of flap and free stream Mach number.

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