• 한국항공우주학회지
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• 제32권4호
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• pp.53-60
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• 2004

F-4E를 모선으로 하는 초소형 위성을 탑재할 수 있는 공중발사체 1단 부스터용 하이브리드 모터의 최적설계를 실시하였다. 설계변수는 포트개수, 초기 산화제 플럭스, 연소실 압력, 그리고 노즐 팽창비 등을 사용하였다. 또한 서로 다른 최적화 알고리듬의 적용 가능성을 검증하기 위하여 구배법 (GBM)과 유전자 알고리듬 (GA) 방법을 각각 사용하였으며, 목적함수의 선택에 따른 최적화 결과의 변화를 살펴보기 위하여 두 가지 종류의 목적함수 (모터 중량과 모터 길이)를 사용하여 그 결과를 상호 비교하였다. 최적화 알고리듬, 그리고 목적함수의 선택과 무관하게 거의 같은 설계결과로 수렴함을 확인하였다. 최적화결과로 설계요구조건을 만족하는 총중량 704.74kg, 1단 길이 3.74m의 하이브리드 모터를 설계 할 수 있었다.

• 한국구조물진단유지관리공학회 논문집
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• 제24권3호
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• pp.26-38
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• 2020

자기 충전형 콘크리트의 배합물 설계는 전형적인 다기준의사결정의 과정이다. 본 연구에서는 실험설계법과 반응표면법을 이용하여 SCC 배합물 전산 설계가 가능하도록 재료성능 및 비용모델을 생성하고, 요구조건을 반영한 여러 성능 사이의 상대적 중요도를 산정하여 가중 다목적 설계문제로 정식화하여 수치최적해를 계산함으로써 비용효율을 고려한 SCC최적설계를 수행하였다. 실험비용과 시간을 고려하여 SCC의 수많은 요구성능 중 압축강도, 철근충전성, 재료분리저항성, 비용정보 등을 다목적 최적화의 목적함수로 설정하였다. 재료경제성을 최적재료설계프로세스에 합리적으로 반영함으로써 경제적 콘크리트배합설계를 수행할 수 있었으며, 본 연구 결과 실험점 계획에서부터 최적해 산출에 이르는 과정을 객관적인 프로세스로 구성함으로써 콘크리트 범용 최적재료설계기술 및 전산화를 기대할 수 있다.

• 한국항공우주학회지
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• 제47권6호
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• pp.460-467
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• 2019

본 논문은 지대지 유도탄 체계의 개념 설계를 위한 다목적 최적화(MOO) 프레임워크를 제안한다. 제안된 프레임워크를 통해 연구 개발 과정의 초기 단계에 체계 수준에서 trade-off를 수행하기 위한 파레토 프론트를 도출 할 수 있다. 제안된 프레임워크는 모델의 추가 및 변경이 용이하도록 네 가지 기능 모듈(환경 설정 모듈, 변수 설정 모듈, 다분야 분석 모듈 및 최적화 모듈)로 구성되었으며, 이를 활용한 개념 설계 프로세스를 통해 개발 초기 단계에 다양한 설계안에 대한 검토를 수행하는 목적을 달성할 수 있었다. 프레임 워크의 효과를 보여주는 사례 연구를 제시하여 체계 설계에 적용 가능성을 확인하였고, 초기 개념 설계 단계에서 신뢰도와 계산시간 감소를 확보할 수 있는 설계 환경을 제시하는데 기여할 수 있었다.

• 한국자동차공학회논문집
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• 제12권2호
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• pp.123-130
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• 2004

The automobile suspension system is composed of parts that affect performances of a vehicle such as ride quality, handling characteristics, straight performance and steering effort, etc. Moreover, by using the finite element analysis the cost for the initial design step can be decreased. In the design of a suspension system, usually system vibration and structural rigidity must be considered simultaneously to satisfy dynamic and static requirements simultaneously. In this paper, we consider the weight reduction and the increase of the first eigen-frequency of a suspension part, the upper control arm, especially using topology optimization and size optimization. Firstly, we obtain the initial design to maximize the first eigen-frequency using topology optimization. Then, we apply the multi-objective parameter optimization method to satisfy both the weight reduction and the increase of the first eigen-frequency. The design variables are varying during the optimization process for the multi-objective. Therefore, we can obtain the deterministic values of the design variables not only to satisfy the terms of variation limits but also to optimize the two design objectives at the same time. Finally, we have executed reliability based optimal design on the upper control arm using the Monte-Carlo method with importance sampling method for the optimal design result with 98％ reliability.

• Computers and Concrete
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• 제14권4호
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• pp.445-462
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• 2014

To solve structural optimization problems, it is necessary to integrate a structural analysis package and an optimization package. There have been many packages that can be employed to analyze reinforced concrete plane frames. However, because most structural analysis packages suffer from closeness of systems, it is very difficult to integrate them with optimization packages. To overcome the difficulty, we proposed a possible alternative, DAMDO, which integrates Design, Analysis, Modeling, Definition, and Optimization phases into an integration environment as follows. (1) Design: first generate many possible structural design alternatives. Each design alternative consists of many design variables X. (2) Analysis: employ the structural analysis software to analyze all structural design alternatives to obtain their internal forces and displacements. They are the response variables Y. (3) Modeling: employ artificial neural networks to build the models Y=f(X) to obtain the relationship functions between the design variables X and the response variables Y. (4) Definition: employ the design variables X and the response variables Y to define the objective function and constraint functions. (5) Optimization: employ the optimization software to solve the optimization problem consisting of the objective function and the constraint functions to produce the optimum design variables. The RC frame optimization problem was examined to evaluate the DAMDO approach, and the empirical results showed that it can be solved by the approach.

• 한국건설관리학회논문집
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• 제17권3호
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• pp.3-12
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• 2016

최근 건설업계의 해외진출이 불가피한 상황에서 국내 설계도면의 경쟁력은 뒤처져있다는 평가를 받고 있다. 따라서 객관적 도면평가를 통해 국내도면수준을 파악하고, 설계경쟁력 확보방안을 마련하고자 한다. 실시설계도면을 기반으로 설계속성을 도출하고, 기존 유사연구와 전문가 인터뷰를 거쳐 속성을 보완한 뒤, 이들을 평가항목으로 Likert척도와 FMEA기법을 이용하여 실무자를 대상으로 설문조사를 실시하였다. 그 결과 국내도면의 상대적 수준에 대한 시공사와 설계사의 의견이 다르고, 중요성을 인지하는 속성이 상이함을 확인하고 그 이유를 분석하였다.

• 한국정밀공학회지
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• 제28권11호
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• pp.1297-1308
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• 2011

The light-weight design of UTM (Urban Transit Maglev)-02 car-body frames are performed, based on initial configuration. The thicknesses of fourteen sub-structures are defined as design variables and the loading condition is considered according to weight of sub-structures, electronic and pneumatic modules and passengers. For efficient and robust process of design optimization, objective function and constraints are approximated by response surface approximation. Structural analysis is performed at some sampling points to construct the approximated objective function and constraints composed of design variables. Design space is changed to find many optimal candidates and best optimal design can be found eventually. The Matlab Optimization Toolbox is used to find optimal value and sensitivity analysis about each design variable is also performed.

• 한국경영과학회:학술대회논문집
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• 대한산업공학회/한국경영과학회 1994년도 춘계공동학술대회논문집; 창원대학교; 08월 09일 Apr. 1994
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• pp.103-111
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• 1994

An interactive and iterative design method based on the constraint satisfaction problem (CSP) technique was developed to generate an ergonomically sound layout of a control panel. This control panel layout method attempts to incorporate a variety of relevant ergonomic principles and design constraints, and generate an optimal or, at least, a "satisfactory" solution through iterative interactions with the designer. The existing panel design and layout methods are mostly based on the optimization of single objective function formulated to reflect and trade off all ergonomic design objectives which are largely different in their nature. In fact, the problem of seeking an ergonomically sound panel design should be viewed as a multiple objective optimization problem. Furthermore, most of the design objectives should be understood as constraints rather than objectives to be optimized. Hence, a constraint satisfaction approach is proposed in this study as a framework for the panel designer to search through the design decision space effectively and make various design decisions iteratively. In order to apply the constraint satisfaction approach to the panel design procedure, the ergonomic principles such as frequency-of-use, importance, functional grouping, and sequence-of-use are formalized as CSP terms. With this formalization, a prototype system was implemented and applied to panel layout problems. The results clearly showed the effectiveness of the proposed approach since it permits designers to consider and iteratively evaluate various design constraints and ergonomic principles, and, therefore, aids the panel designer to come up with an ergonomically sound control panel layout.

• 한국자동차공학회논문집
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• 제19권6호
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• pp.1-9
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• 2011

In this study, the specifications of the components of the vent vale were optimally determined in order to enhance the performance of the vent valve. Design objective was to minimize fuel leakage while satisfying the design constraints on the performance indices. To obtain the optimum solution based on real experiments, several design techniques available in PIAnO, a commercial PIDO tool, were used. First, an orthogonal array was used to generate training design points and then real experiments were performed to measure the experimental data at the training design points. Next, Kriging metamodels for the objective function and design constraints were generated using the experimental data. Finally, a genetic algorithm was employed to obtain the optimization results using the Kriging models. Fuel leakage of the optimized vent valve was found to be reduced by 95.8% compared to that of the initial one while satisfying all the design constraints.

• 한국공간구조학회논문집
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• 제1권1호
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• pp.125-134
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• 2001

The objective of this study is the development of size discrete optimum design algorithm which is based on the GAs(genetic algorithms). The algorithm can perform size discrete optimum designs of space trusses. The developed algorithm was implemented in a computer program. For the optimum design, the objective function is the weight of space trusses and the constraints are limite state design codes(1998) and displacements. The basic search method for the optimum design is the GAs. The algorithm is known to be very efficient for the discrete optimization. This study solves the problem by introducing the GAs. The GAs consists of genetic process and evolutionary process. The genetic process selects the next design points based on the survivability of the current design points. The evolutionary process evaluates the survivability of the design points selected from the genetic process. In the genetic process of the simple GAs, there are three basic operators: reproduction, cross-over, and mutation operators. The efficiency and validity of the developed discrete optimum design algorithm was verified by applying GAs to optimum design examples.