• Journal of the Computational Structural Engineering Institute of Korea
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• v.16 no.1
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• pp.59-68
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• 2003

An optimization Program is developed to produce new topologies of plane structures under multiload case. A four-node finite element is used in the response analysis to reduce the computation time and to ultimately achieve practical topology optimization. The bilinear finite element is prone to produce chequer-boarding phenomenon and a simple filtering process is therefore adopted. An artificial material model is employed to represent the structural material and the resizing algorithm based on the optimality criteria is adopted to update the material density parameter during optimization process. With newly developed optimization program, the comparison study has been made between single and multiload cases and its results are described in this paper. From numerical results, it appears that multiload case should be considered to achieve the practical topology optimization.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.174.2-174.2
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• 2012

위성의 방열판 설계 과정은 수치해석을 위해 위성을 모델링한 열모델에서 분할 격자인 노드를 기준으로 방열판 위치와 형상, 크기를 조절하면서 한계 온도조건을 만족할 때까지 설계 엔지니어의 판단에 의존하여 열해석을 반복하는 것이 보편적인 방식이다. 대부분 방열판 면적을 줄이기 위한 추가적인 노력을 하지 않기 때문에 필요 이상의 과도한 방열판 설계를 하는 경우가 많은 것이 사실이다. 이러한 방열판 설계에서 최소한의 방열판 면적을 사용하여 한계 온도를 만족하도록 설계를 최적화 한다면 무엇보다 전체 위성 열설계의 효율성과 경제성을 높일 수 있는 바탕이 될 수 있을 것이다. 위성의 방열판 설계는 방열판 영역 내에서 동일한 면적을 가지더라도 위치나 형상에 따라 그 효과가 상당히 차이가 날 수 있기 때문에 실제 방열판 설계에서는 이러한 점을 고려하는 것이 필수적이다. 먼저 위성은 열해석에 알맞는 격자 크기로 분할된 노드로 이루어진 열모델로 모델링되어 개발된다. 방열판이 설계되는 방열판 영역 역시 격자 모양의 노드로 분할되기 때문에 열해석을 이용하여 방열판 설계를 한다면 노드 크기를 기준으로 노드 분할 형태에 따라 설계를 한다. 그래서 위성 열모델에서 방열판 영역의 각 노드가 방열판 노드 여부에 따라 모자이크와 같은 분포의 방열판 설계를 하게 되므로 방열판 노드 분포의 최적화가 방열판 최적 설계를 의미하게 된다. 본 연구에서는 방열판 설계 최적화를 위해 일반적인 위성 프로그램의 열제어 개발에서 사용하는 위성 열모델과 열해석 프로그램을 최적화 기법과 동일한 언어로 다시 개발해야 하는 부담 없이 그대로 최적화 기법과 연동할 수 있도록 하는 방법을 제안하고, 실제 소형의 검증용 위성 열모델을 개발하여 여러 가지 해석 조건에 따른 방열판 최적 설계 결과를 비교하고 검토함으로써 이러한 접근 방식을 검증해보고자 하였다.

• The Transactions of the Korea Information Processing Society
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• v.6 no.6
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• pp.1542-1555
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• 1999

This paper proposes an algorithm for class hierarchies which can optimize member data and member function. This algorithm considers single/multiple inheritance, static/dynamic binding, overloading/overriding, pure virtual/virtual function, and constructor on the hierarchy of C++ class. We need to eliminate unused function that possesses many component element, because the program uses a limited of function in class hierarchies. Previous works on slicing mainly focused on selecting output data and including the related program statement. It was consists of structured programming language and also centralized on error detection, maintenance, and flexible testing. In this paper, we extend to the object-oriented language, makes a linked-table for objects to raise the efficiency of information management, and proposes necessary algorithm for optimizing system Through this process, we can obtain the simplification of program code and the progress of system performance by eliminating unused member data and member function.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2008.05a
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• pp.734-737
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• 2008

This paper presents a new automatic TFT-LCD image quality optimization system. We also have developed new algorithms using 6-point programmable matching technique with reference gamma curve, and automatic power setting sequence. It optimizes automatically gamma adjustment and power setting registers in mobile TFT-LCD driver IC to reduce gamma correction error, adjusting time, and flicker. Developed algorithms and programs are generally applicable for most of the TFT-LCD modules. The proposed optimization system contains module-under-test (MUT, TFT-LCD module), control program, multimedia display tester for measuring luminance and flicker, and control board for interface between PC and TFT-LCD module. The control board is designed with DSP, and it supports various interfaces such as RGB and CPU. Developed automatic image quality optimization system showed significantly reduced gamma adjusting time, reduced flicker, and much less average gamma error than competing system. We believe that the proposed system is very useful to provide high image quality TFT-LCD and to reduce developing process time using optimized gamma-curve setting and automatic power setting.

• Fire Science and Engineering
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• v.28 no.3
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• pp.1-9
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• 2014

In this study, it was developed to the design program optimization the design factors of the carbon dioxide fire extinguishing system on the basis of design theory for the carbon dioxide fire extinguishing system, national emergency management agency (NEMA) notice No. 2012-11, KS B 6261 and steepest descent method of optimization. The design program was developed to C++ compiler based on established the logic and algorithms and was to operate on the Windows operating system. The optimization of design factors for the carbon dioxide fire extinguishing system are minimized subject to constraint on agent flow rate, emission time and design variables (pipe size etc.). It was verified to the design program performance for test system, and it was provided to the foundation for optimal design in fire fighting field. Also, it is considered to improve the efficiency of the fire extinguishing system and to maximize of fire suppression as the construction of the carbon dioxide extinguishing system based on the optimal design factors.

• The Journal of Korean Association of Computer Education
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• v.10 no.1
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• pp.67-75
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• 2007

The purpose of the study is to develop handheld learning tool based on design principles drawn from cognitive load theory. To optimize learner's cognitive load, the learning program should be developed for maximizing the effective load and(or) minimizing ineffective load. The principles, which were applied to developing the learning program, for minimizing the extraneous cognitive load, one of the ineffective loads, are modality, redundancy, split-attention, multimedia, and worked-out example. In this study, we will show possibilities for designing an effective mobile learning program.

• Journal of the Korean Society of Propulsion Engineers
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• v.13 no.6
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• pp.24-33
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• 2009

The present study deals with the optimization of the leading edge shape around a wing-body junction to minimize the strength of the horseshoe vortex, which is one of the main factor generating the secondary flow losses. For this purpose, approximate optimization method is used for the optimization. The study is performed by using $FLUENT^{TM}$ and $iSIGHT^{TM}$. The total pressure coefficient for the optimized model was decreased about 9.79% compared with the baseline model.

• Proceedings of the Korean Information Science Society Conference
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• 2001.04a
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• pp.55-57
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• 2001

자바언어는 이질적인 네트워크 환경에서 프로그램 개발이 적합하도록 설계된 언어이다. 자바언어의 특징은 소프트웨어를 쉽게 개발하는데 유용한 것은 사실이지만, 성능상 제약이 따르게 된다. 즉 자바는 클래스 파일이 이동하여 JVM 환경에서 인터프리팅 되는 시스템이므로, 클래스 파일이 이동하며 실행되는 동안의 성능의 저하 없이 자바의 특징을 이용하려면 복잡한 최적화와 실행 시스템이 요구된다. 본 논문은 네트워크 상에서 동적으로 다운로드 되는 클래스 파일의 최적화에 있다. 클래스 파일이 인터프리팅 되는 시스템이 보다 적은 네트워크 로드를 가지고 실행할 수 있도록 하며, 효율적인 실행 속도를 보이도록 하는 것이다. 여기서는 Class Field Optimizer는 내부적으로 Bytecode Optimizer와 ClassGen을 이용하여 실행시간을 개선하고 전체 클래스 파일의 크기를 줄이게 된다. Bytecode Optimizer는 peephole 최적화를 수행하고, bytecode 의존적 최적화, 그리고 전역최적화를 행하게 된다. ClassGen은 클래스 파일의 포맷에 따라 bytecode를 분석하고 본래의 클래스 파일보다 작은 크기의 클래스 파일을 생성하게 된다. 최적화된 클래스 파일은 부분적으로 클래스 파일의 최적화를 가져와 전체 클래스 파일의 크기를 줄이고, 인터프리터를 통하여 실행될 때 수행 속도면에서 좀더 빠른 실행 속도를 가지게 된다.

• Journal of Korean Society of Steel Construction
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• v.21 no.2
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• pp.193-201
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• 2009

Structural design of most nonprismatic Pre-Engineered Building Systems (PEBS) is performed using optimizing software developed in foreign countries. In this study, a structural optimizing software for the design of 3-D structures of nonprismatic PEBS is developed according to the allowable stress design method of AISC2005 and KBC. Optimizing structural design with nonprismatic members is carried out by repeating the process of structural analysis and member design to minimize the weight of a structure. According to the optimizing design results of 2-D and 3-D structures with nonprismatic members, there are considerable steel savings in designing structures with nonprismatic H-shaped built-up sections rather than with H-shaped rolled sections. When H-shaped built-up sections were used, the weight of the structural steel was reduced when AISC2005 specification rather than AISC1898 was used in the design. It is therefore concluded that utilizing the new AISC2005 specification is safer in preventingweb buckling because the height of a member is designed to be small despite some differences depending on the structural type.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.32 no.10
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• pp.12-19
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• 2004

An aerodynamic design optimization system for three-dimensional wing was developed as a part of the future MDO framework. The present design optimization system includes four modules such as geometry design, grid generation, flow solver and optimizer. All modules were based on commercial softwares and programmed to have automated execution capability in batch mode utilizing built-in script and journaling. The integration of all modules into the system was accomplished through programming using Visual Basic language. The distributed computational environment based on network communication was established to save computational time especially for time-consuming aerodynamic analyses. The distributed aerodynamic computations were performed in conjunction with the global optimization algorithm of response surface method, instead of using usual parallel computation based on domain decomposition. The application of the design system in the drag minimization problem demonstrated considerably enhanced efficiency of the design process while the final design showed reasonable results of reduced drag.