• 한국항공운항학회지
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• 제21권1호
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• pp.30-38
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• 2013

This paper describes the design optimization of Unmanned Aerial Vehicles(UAVs). An optimization framework has been developed and implemented for the conceptual design of UAVs. An integrated design analysis program was developed with several analysis modules such as propulsion, performance, mission, weight, and stability and control. A UAV configuration design optimization was performed by implementing the integrated analysis to enhance the endurance of UAVs. A SQP optimizer was utilized to build an optimization module for this program and sensitivity analysis was performed to determine the trends of shape variables for developing optimization objective. In conclusion, the results indicate that the resulting optimized UAVs configurations show performance improvements over the baseline design and reliable analysis results.

• 한국정보과학회:학술대회논문집
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• 한국정보과학회 2000년도 봄 학술발표논문집 Vol.27 No.1 (A)
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• pp.56-58
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• 2000

자바 클래스 파일은 각 플랫폼에 독립적인 중간 코드 형태의 바이트코드와 자료 구조로 구성됨으로서 네트워크를 통하여 플랫폼에 독립적으로 인터프리티브 컴파일링 시스템에서 실행된다. 그러나 클래스 파일을 생성하는 자바 컴파일러는 각 플랫폼에 독립적인 바이트코드 표현에 제약을 받기 때문에 효율적인 코드를 생성하는데 한계가 있다. 또한, 자바 가상 기계에서 동적 링킹을 지원하기 위하여 고안된 상수 풀(constant pool)의 크기가 상대적으로 큰 특징을 갖는다. 따라서 자바 클래스 파일이 네트워크와 같은 실행 환경에서 효과적으로 실행되기 위해서는 작은 크기와 효율적인 코드에 대한 변환이 요구된다. 본 논문에서는 자바 클래스 파일이 인터넷 및 분산환경 시스템에서 효율적으로 실행되기 위해서 클래스 파일의 크기를 줄이는 방법과 자바 컴파일러가 생성한 바이트코드에 대해 최적화를 수행하는 최적화 방법론을 제시하고, 코드 최적화기를 설계한다. 최적화된 클래스 파일은 코드 크기를 줄이고, 효율적인 코드를 생성함으로서 네트워크상의 전송 속도뿐만 아니라 가상 기계에서 좀 더 빠르게 실행할 수 있다.

• 한국자동차공학회논문집
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• 제4권1호
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• pp.110-122
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• 1996

The objective of this study is to understand the dynamic characterictics of OHV type valve trains and to design and optimal cam profile which will improve engine performance. A numerical model for valve train dynamics is presented, which aims at both accuracy and computational efficiency. The lumped mass model and distributed parameter model were used to describe the valve train dynamics. Nonlinear characterictics in the valve spring behavior were included in the model. Comprehensive experiments were carried out concerning the valve train dynamics, and the model was tuned based on the test results. The dynamic model was used in designing an optimal cam profile. Because the objective function has many local minima, a conventional local optimizer cannot be used to find an optimal solution. A modified adaptive random search method is successfully employed to solve the problem. Cam lobe area could be increased up to 7.3% without any penalties in kinematic and dynamic behaviors of the valve train.

• International Journal of Aeronautical and Space Sciences
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• 제14권4호
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• pp.334-340
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• 2013

This paper deals with the optimization of blade stiffened composite panels. The main objective of the research is to make response surfaces for the constraints. The response surface for warping thermal deformation was previously made for a fixed dimension composite structure. In this study, the dimensions of the blade stiffener were treated as design variables. This meant that a new response surface technique was required for the constraints. For the response surfaces, the lamination parameters, linear thermal expansions and dimensions of the structures were used as variables. A genetic algorithm was adopted as an optimizer, and an optimal result, which satisfied two constraints, was obtained. As a result, a new response surface was obtained, for predicting warping thermal deformation.

• 인터넷정보학회논문지
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• 제19권4호
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• pp.35-44
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• 2018

Monitoring through Synthesis Aperture Radar (SAR) is responsible for marine safety from floating icebergs. However, there are limits to distinguishing between icebergs and ships in SAR images. Convolutional Neural Network (CNN) is used to distinguish the iceberg from the ship. The goal of this paper is to increase the accuracy of identifying icebergs from SAR images. The metrics for performance evaluation uses the log loss. The two-layer CNN model proposed in research of C.Bentes et al.[1] is used as a benchmark model and compared with the four-layer CNN model using data augmentation. Finally, the performance of the final CNN model using the VGG-16 pre-trained model is compared with the previous model. This paper shows how to improve the benchmark model and propose the final CNN model.

• 항공우주기술
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• 제10권1호
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• pp.175-182
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• 2011

100인승 이하의 쌍발 터보프롭 항공기의 날개 형상에 대한 최적 설계를 수행하였다. 최적설계는 2단계로 이뤄져 있는데 먼저 꼬리날개의 높이에 대한 방향안정성을 분석하였고 방향 안정성을 갖는 높이에 대해 순항조건에 대해 항력을 최소로 하는 날개의 최적형상을 결정하였다. 방향안정성 분석은 Vorstab를 통해 이뤄졌고, 최적형상은 Piano를 활용하여 결정하였으며 공력해석은 점성을 고려한 Fluent 코드를 활용하였다. 최적설계 결과 약 10 count의 항력을 감소하였다.

• Structural Engineering and Mechanics
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• 제5권1호
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• pp.59-68
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• 1997

A two-step method is presented for the optimum design of trusses with available sections under stress and Euler buckling constraints. The shape design of the truss is used as a means to convert the discrete solution into a continuous one. In the first step of the method, a continuous solution is obtained by sizing and shape design using an approximate polynomial expression for the buckling coefficients. In the second step, the member sizes obtained are changed to the nearest available sections and the truss is reconfigured by using the exact values for the buckling coefficients. The optimizer used is based on the sequential quadratic programming and the gradients are evaluated in closed form. The method is illustrated by two numerical examples.

• 경영과학
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• 제21권2호
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• pp.43-60
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• 2004

Every iteration of interior-point methods of large scale optimization requires computing at least one orthogonal projection. In the practice, symmetric variants of the Gaussian elimination such as Cholesky factorization are accepted as the most efficient and sufficiently stable method. In this paper several specific implementation issues of the symmetric factorization that can be applied for solving such equations are discussed. The code called McSML being the result of this work is shown to produce comparably sparse factors as another implementations in the $MATLAB^{***}$ environment. It has been used for computing projections in an efficient implementation of self-regular based interior-point methods, McIPM. Although primary aim of developing McSML was to embed it into an interior-point methods optimizer, the code may equally well be used to solve general large sparse systems arising in different applications.

• 한국정보과학회:학술대회논문집
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• 한국정보과학회 1998년도 가을 학술발표논문집 Vol.25 No.2 (1)
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• pp.36-38
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• 1998

객체지향 데이터베이스 시스템의 표준 질의어로 사용되는 OQL은 SQL과 달리 select-from-where절 어디서나 중첩 질의를 자유롭게 허용하며, 이러한 중첩 질의는 질의어 수행 성능에 중요한 영향을 미치므로, OQL을 처리하는 질의 처리기에서는 이를 반드시 고려해 주어야 한다. 본 논문은 모노이드 컴프리핸션 해석(monoid comprehension calculus)을 이용하여, OQL 질의 처리기에서 중첩 질의의 중첩 구조를 제거할 수 있도록 해주고, 나아가 기존 질의 처리기에서 중첩질의 처리 기능을 추가하는데 있어, 이미 구현되어 있는 질의 최적화 모듈과 질의 수행 모듈의 수정을 최소화할 수 있는 중첩 질의 구조 제거용 전위 모듈(unnesting front-end)을 설계하고 구현하였다.

• Smart Structures and Systems
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• 제20권5호
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• pp.607-618
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• 2017

In this research, a newly developed nature-inspired optimization method, the Lion Pride Optimization algorithm (LPOA), is utilized for optimal design of composite steel box girder bridges. A composite box girder bridge is one of the common types of bridges used for medium spans due to their economic, aesthetic, and structural benefits. The aim of the present optimization procedure is to provide a feasible set of design variables in order to minimize the weight of the steel trapezoidal box girders. The solution space is delimited by different types of design constraints specified by the American Association of State Highway and Transportation Officials. Additionally, the optimal solution obtained by LPOA is compared to the results of other well-established meta-heuristic algorithms, namely Gray Wolf Optimization (GWO), Ant Lion Optimizer (ALO) and the results of former researches. By this comparison the capability of the LPOA in optimal design of composite steel box girder bridges is demonstrated.