• International Journal of Aeronautical and Space Sciences
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• 제8권1호
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• pp.66-78
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• 2007

A multi-point aerodynamic shape optimization technique has been developed for helicopter rotor blades in hover based on a continuous adjoint method on unstructured meshes. The Euler flow solver and the continuous adjoint sensitivity analysis were formulated on the rotating frame of reference. The 'objective function and the sensitivity were obtained as a weighted sum of the values at each design point. The blade section contour was modified by using the Hicks-Henne shape functions. The mesh movement due to the blade geometry change was achieved by using a spring analogy. In order to handle the repeated evaluation of the design cycle efficiently, the flow and adjoint solvers were parallelized based on a domain decomposition strategy. A solution-adaptive mesh refinement technique was adopted for the accurate capturing of the wake. Applications were made to the aerodynamic shape optimization of the Caradonna-Tung rotor blades and the UH-60 rotor blades in hover.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 춘계학술대회
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• pp.1783-1788
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• 2003

In this study, the image processing program for deducing parameters of the elliptic shape of the partially overlapped liquid droplets was developed using the randomized Hough transform and the parameter decomposition. The procedure for the shape detection consists of three steps. For the first step, the candidate centers of ellipses are determined by the geometric property of the ellipse. Next, the rest parameters are estimated by the randomized Hough transform. In the final step for the post-processing, optimally approximated parameters of ellipses are determined. The developed program was applied to the simulated overlapped ellipses, real overlapped droplets, and real spray droplets. The shape detection was very excellent unless there existed inherent problems in original images. Moreover, this method can be used as an effective separating method for the overlapped small particles.

• 한국통신학회논문지
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• 제24권9A호
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• pp.1419-1424
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• 1999

형태학적 필터를 영상 처리 시스템에 효율적으로 구현하기 위하여서는 영상 처리 시스템의 구조적인 제약으로 인하여 형태소의 크기가 작아야 하며, 따라서 크기가 큰 형태소를 가지는 필터의 구현을 위하여 주어진 형태소를 작은 크기의 형태소로 분해하는 과정이 필요하다. 본 논문에서는 임의의 형태학적 필터를 3$\times$3 Pipeline Machine에 효율적으로 구현하기 위하여 모양과 크기에 아무 제한 없이 행태소를 분해하는 알고리즘을 개발한다. 먼저 주어진 형태소를 순차적 방법으로 합집합 분해하고, 각 분해된 결과를 다시 3$\times$3 크기의 형태소로 최적 분해하여 최종 형태소 분해 결과를 얻는다. 개발된 분해 알고리즘을 형태소에 적용하여 분해 결과를 구하였으며, 최적에 매우 근접한 결과를 얻을 수 있었다.

• 대한원격탐사학회지
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• 제28권6호
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• pp.623-632
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• 2012

In this paper, we analyzed the effect of wavelet decomposition levels in feature extraction for anomaly detection from hyperspectral imagery. After wavelet analysis, anomaly detection was experimentally performed using the RX detector algorithm to analyze the detecting capabilities. From the experiment for anomaly detection using CASI imagery, the characteristics of extracted features and the changes of their patterns showed that radiance curves were simplified as wavelet transform progresses and H bands did not show significant differences between target anomaly and background in the previous levels. The results of anomaly detection and their ROC curves showed the best performance when using the appropriate sub-band decided from the visual interpretation of wavelet analysis which was L band at the decomposition level where the overall shape of profile was preserved. The results of this study would be used as fundamental information or guidelines when applying wavelet transform to feature extraction and selection from hyperspectral imagery. However, further researches for various anomaly targets and the quantitative selection of optimal decomposition levels are needed for generalization.

• 한국항공우주학회지
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• 제47권7호
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• pp.535-540
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• 2019

MDO(Multi-disciplinary Optimization)를 위한 서로 다른 모델 간의 결합은 계산 프레임 워크의 복잡성을 크게 증가시키는 동시에 CPU 시간과 메모리 사용을 증가시킨다. 이러한 어려움을 극복하기 위해 POD(Proper Orthogonal Decomposition)와 RBF(Radial Basis Function)를 사용하여 복합 샌드위치 구조가 항공기 날개 스킨 재료로 사용될 때 복합재와 샌드위치 코어의 두께를 결정하는 최적화 문제의 해를 구했다. POD와 RBF를 사용하여 날개 형상과 하중 데이터에 대한 대리 모델을 만들었으며 대리 모델에 의해 얻어진 목적 함수 및 제약 함수 값을 사용하여 최적해를 구하였다.

• 한국응용과학기술학회지
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• 제17권1호
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• pp.55-61
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• 2000

$Zn_{x}Fe_{3-x}O_{4}(0.00.<X<0.08)$ was synthesized by air oxidation method for the decomposition of carbon dioxide. We investigated the characteristics of catalyst, the form of methane by gas chromatograph after decomposition of carbon dioxide and kinetic parameter. $Zn_{x}Fe_{3-x}O_{4}(0.00.<X<0.08)$ was spinel type structure. The surface areas of catalysts($Zn_{x{Fe_{3-x}O_{4}(0.00.<X<0.08)$) were $15{\sim}27$ $m^{2}/g$. The shape of $Zn_{0.003}Fe_{2.997}O_{4}$ was sphere. The optimum temperature for the decomposition of carbon dioxide into carbon was $350^{\circ}C$. $Zn_{0.003}Fe_{2.997}O_{4}$ showed the 85% decomposition rate of carbon dioxide and the degree of reduction by hydrogen(${\delta}$) of $Zn_{0.003}Fe_{2.997}O_{4}$ was 0.32. At $350^{\circ}C$, the reaction rate constant and activation energy of $Zn_{0.003}Fe_{2.997}O_{3.68}$ for the decomposition of carbon dioxide into carbon were 3.10 $psi^{1-{\alpha}}/min$ and 0.98 kcal/mole respectively. After the carbon dioxide was decomposed, the carbon which was absorbed on the catalyst surface was reacted with hydrogen and it became methane.

• Structural Engineering and Mechanics
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• 제8권1호
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• pp.73-84
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• 1999

This paper is concerned with shape optimization problems by the boundary element method (BEM) emphasizing the use of a reduced basis reanalysis technique proposed recently by the author. Problems of this class are conventionally carried out iteratively through an optimizer; a sequential quadratic programming-based optimizer is used in this study. The iterative process produces a succession of intermediate designs. Repeated analyses for the systems associated with these intermediate designs using an exact approach such as the LU decomposition method are time consuming if the order of the systems is large. The newly developed reanalysis technique devised for boundary element systems is utilized to enhance the computational efficiency in the repeated system solvings. Presented numerical examples on optimal shape design problems in electric potential distribution and elasticity show that the new reanalysis technique is capable of speeding up the design process without sacrificing the accuracy of the optimal solutions.

• 한국정보통신학회:학술대회논문집
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• 한국해양정보통신학회 1999년도 춘계종합학술대회
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• pp.185-191
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• 1999

Mathematical morphology based on set theory has been applied to various areas in image processing. Pitas proposed a object recognition algorithm using Morphological Shape Decomposition(MSD), and a new representation scheme called Morphological Shape Representation(MSR). The Pitas's algorithm is a simple and adequate approach to recognize objects that are rotated 45 degree-units with respect to the model object. However, this recognition scheme fails in case of random rotation. This disadvantage may be compensated by defining small angle increments. However, this solution may greatly increase computational complexity because the smaller the step makes more number of rotations to be necessary. In this paper, we propose a new method for object recognition based on MSD. The first step of our method decomposes a binary shape into a union of simple binary shapes, and then a new tree structure is constructed which ran represent the relations of binary shapes in an object. finally, we obtain the feature informations invariant to the rotation, translation, and scaling from the tree and calculate matching scores using efficient matching measure. Because our method does not need to rotate the object to be tested, it could be more efficient than Pitas's one. MSR has an intricate structure so that it might be difficult to calculate matching scores even for a little complex object. But our tree has simpler structure than MSR, and easier to calculated the matchng score. We experimented 20 test images scaled, rotated, and translated versions of five kinds of automobile images. The simulation result using octagonal structure elements shows 95% correct recognition rate. The experimental results using approximated circular structure elements are examined. Also, the effect of noise on MSR scheme is considered.

• 정보처리학회논문지B
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• 제10B권2호
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• pp.135-142
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• 2003

본 논문은 영상내 객체정보의 정확한 복원을 위하여, 연속된 2차원 영상으로부터 특정 객체의 특징점을 추출하고, 특징점의 위치 데이터들로부터 원형의 3차원 모양 및 모션 정보를 복원하는 알고리즘과 결과를 제시하였다. 2차원 영상의 특징점 검출을 위해서는 물체와 배경이 명확히 구별되는 실험영상 환경에서 색상변환을 통한 자동 추출 방법을 사용하였다. 추출된 2차원 객체의 특징점들로부터 3차원 모앙, 움직임 정보를 복원하기 위하여 스테레오 카메라와 준원근 카메라 모델을 적용하고 SVD(SinEuiar Value Decomposition)에 의한 인수분해연산을 수행하였다. 준원근 카메라 모델의 근본적인 문제인 깊이정보의 복원 에러가, 스테리오 영상 분석에 의해 최소화 되었다. 본 논문에서 제시된 방법들의 성능을 객관적으로 평가하기 위하여 크기와 위치가 알려진 3차원 물체에 대해 실험을 행하였으며, 영상의 21개 특징점 위치와 공간상에서의 3개 방향으로의 움직임 각도를 연산에 의해 복원한 후 원형의 데이터와 비교하여 본 알고리즘의 정확성을 증명하였다.

• Journal of Mechanical Science and Technology
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• 제14권8호
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• pp.867-878
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• 2000

In order to study unsteady aerodynamic loads on high speed trains passing by each other 350km/h, three-dimensional flow fields around trains during the crossing event are numerically simulated using three-dimensional Euler equations. Roe's FDS with MUSCL interpolation is employed to simulate wave phenomena. An efficient moving grid system based on domain decomposition techniques is developed to analyze the unsteady flow field induced by the restricted motion of a train on a rail. Numerical simulations of the trains passing by on the double-track are carried out to study the effect of the train nose-shape, length and the existence of a tunnel on the crossing event. Unsteady aerodynamic loads-a side force and a drag force-acting on the train during the crossing are numerically predicted and analyzed. The side force mainly depends on the nose-shape, and the drag force depends on tunnel existence. Also. a push-pull (i.e.impluse force) force successively acts on each car and acts in different directions between the neighborhood cars. The maximum change of the impulsive force reaches about 3 tons. These aerodynamic force data are absolutely necessary to evaluate the stability of high speed multi-car trains. The results also indicate the effectiveness of the present numerical method for simulating the unsteady flow fields induced by bodies in relative motion.