• Composites Research
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• 제21권1호
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• pp.30-39
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• 2008

본 논문에서는 기존의 유전자 알고리즘을 대신하여 병렬 마이크로 유전자 알고리즘을 사용한 복합재료 적층 구조물의 최적설계를 수행하였다. 마이크로 유전자 알고리즘은 한 세대 당 보통 5개의 개체로 해를 탐색한다 비록 세대를 구성하는 인구수는 적지만 공칭수렴 판단과 재초기화 과정을 통해 다양성을 제공하기 때문에 최적해 탐색이 가능하다. 2가지의 복합재 구조물의 최적화 문제를 가정하고 이를 마이크로 유전자 알고리즘을 사용하여 해를 구하였다. 효율성 판단을 위해서 기존의 유전자 알고리즘과 결과를 비교하였다. 두 문제 모두 마이크로 유전자 알고리즘이 비슷한 결과를 도출하면서도 약 70%의 계산량 감소를 보였다. 마이크로 유전자 알고리즘을 사용하여 일정 범위 내에서 변하는 하중을 받고 있는 복합재 적층 구조물의 최적설계를 수행하였다. 계산 결과 고정된 하중상태 하에서 얻은 최적해보다 하중 변화에 덜 민감한 설계변수를 얻을 수 있었다. 이상의 문제를 통해 다양한 설계변수를 갖는 복합재 적층 구조물의 최적설계의 한 방법으로서 마이크로 유전자 알고리즘이 효율적임을 확인하였다.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2005년도 추계학술발표대회 논문집
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• pp.268-271
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• 2005

Researches based on genetic algorithms have been performed in composite laminated structures optimization since 1990. However, conventional genetic algorithms have a disadvantage that its augmentation of calculation costs. A lot of variations have been proposed to improve the performance and efficiency, and micro genetic algorithm is one of them. In this paper, micro Genetic Algorithm was employed in the optimization of laminated stiffened composite structures to maximize the linear critical buckling load and the results from both conventional genetic algorithm and micro genetic algorithm were compared.

• 한국자동차공학회논문집
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• 제12권3호
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• pp.51-58
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• 2004

Optimization of engine desist and operation parameters using a genetic algorithm was demonstrated for direct injection diesel engine combustion. A micro genetic algorithm and a modified KIVA-3V code were used for the analysis and optimization of the engine combustion. At each generation of the optimization step the micro genetic algorithm generated five groups of parameter sets, and the five cases of KIVA-3V analysis were to be performed either in series or in parallel. The micro genetic algorithm code was also parallelized by using MPI programming, and a multi-CPU parallel supercomputer was used to speed up the optimization process by four times. An example case for a fixed engine speed was performed with six parameters of intake swirl ratio, compression ratio, fuel injection included angle, injector hole number, SOI, and injection duration. A simultaneous optimization technique for the whole range of engine speeds would be suggested for further studies.

• 산업공학
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• 제20권4호
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• pp.504-514
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• 2007

The multicast routing problem lies in the composition of a multicast routing tree including a source node and multiple destinations. There is a trade-off relationship between cost and delay, and the multicast routing problem of optimizing these two conditions at the same time is a difficult problem to solve and it belongs to a multi-objective optimization problem (MOOP). A multi-objective genetic algorithm (MOGA) is efficient to solve MOOP. A micro-genetic algorithm(${\mu}GA$) is a genetic algorithm with a very small population and a reinitialization process, and it is faster than a simple genetic algorithm (SGA). We propose a multi-objective micro-genetic algorithm (MO${\mu}GA$) that combines a MOGA and a ${\mu}GA$ to find optimal solutions (Pareto optimal solutions) of multicast routing problems. Computational results of a MO${\mu}GA$ show fast convergence and give better solutions for the same amount of computation than a MOGA.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2006년도 춘계학술대회논문집
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• pp.696-702
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• 2006

Flutter characteristics of composite curved wing were investigated in this study. The efficient and robust system for the flutter optimization of general composite curved wing models has been developed using the coupled computational method based on both the standard genetic algorithm and the micro genetic algorithms. Micro genetic algorithm is used as an alternative method to overcome the relatively poor exploitation characteristics of the standard genetic algorithm. The present results show that the micro genetic algorithm is more efficient in order to find optimized lay-ups for a composite curved wing model. It is found that the flutter stability of curved wing model can be significantly increased using composite materials with proper optimum lamination design when compared to the case of isotropic wing model under the same weight condition.

• Composites Research
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• 제23권4호
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• pp.14-20
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• 2010

본 연구에서는 마이크로 유전자 알고리즘을 이용하여 외부 수압을 받는 필라멘트 와인딩 복합재 원통의 최적설계를 수행하였다. 목적함수는 파손하중과 좌굴하중을 동시에 고려하여 설계하중을 최대화하는 것이다. 좌굴 및 파손해석은 MSC.NASTRAN을 이용하였고, Carroll의 공개된 마이크로 유전자 알고리즘에 기초한 최적화작업을 수행하였다. 설계변수로는 헬리컬(helical) 와인딩 각도와 후프(hoop) 와인딩 층의 두께비가 고려되었다. 본 연구를 통해 마이크로 유전자 알고리즘을 이용하여 다양한 형상을 갖는 필라멘트 와인딩 복합재 원통의 좌굴 및 파손하중 최적화가 가능함을 확인하였고, 제안된 알고리즘이 일반 유전자 알고리즘과 비교해서도 높은 효율을 보였다.

• 한국공작기계학회논문집
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• 제12권3호
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• pp.82-88
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• 2003

SGA(Single Genetic Algorithm) is a heuristic global optimization method based on the natural characteristics and uses many populations and stochastic rules. Therefore SGA needs many function evaluations and takes much time for convergence. In order to solve the demerits of SGA, ${\mu}GA$(Micro-Genetic Algorithm) has recently been developed. In this study, ${\mu}GA$ which have small populations and fast convergence rate, was applied to structural optimization with discrete or integer variables such as 3, 10 and 25 bar trusses. The optimized results of ${\mu}GA$ were compared with those of SGA. Solutions of ${\mu}GA$ for structural optimization were very similar or superior to those of SGA, and faster convergence rate was obtained. From the results of examples, it is found that ${\mu}GA$ is a suitable and very efficient optimization algorithm for structural design.

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 2003년도 춘계학술대회 논문집
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• pp.9-14
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• 2003

SGA (Single Genetic Algorithm) is a heuristic global optimization method based on the natural characteristics and uses many populations and stochastic rules. Therefore SGA needs many function evaluations and takes much time for convergence. In order to solve the demerits of SGA, $\mu$GA(Micro-Genetic Algorithm) has recently been developed. In this study, $\mu$GA which have small populations and fast convergence rate, was applied to structural optimization with discrete or integer variables such as 3, 10 and 25 bar trusses. The optimized results of $\mu$GA were compared with those of SGA. Solutions of $\mu$GA for structural optimization were very similar or superior to those of SGA, and faster convergence rate was obtained. From the results of examples, it is found that $\mu$GA is a suitable and very efficient optimization algorithm for structural design.

• International Journal of Fuzzy Logic and Intelligent Systems
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• 제4권3호
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• pp.283-287
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• 2004

In this paper, a method of designing the efficient batch blind equalization with low complexity using a micro genetic algorithm (GA), is presented. In general, the blind equalization techniques that are focused on the complexity reduction might be carried out with minor effect on the performance. Among the advanced various subjects in the field of GAs, a micro genetic algorithm is employed to identity the unknown channel impulse response in order to reduce the search space effectively. A new cost function with respect to the constant modulus criterion is suggested considering its relation to the Wiener criterion. We provide simulation results to show the superiority of the proposed techniques compared to other existing techniques.

• International Journal of Automotive Technology
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• 제8권5호
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• pp.563-573
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• 2007

Optimal design of an automotive catalytic converter for minimization of cold-start emissions is numerically performed using a micro genetic algorithm for two optimization problems: optimal geometry design of the monolith for various operating conditions and optimal axial catalyst distribution. The optimal design process considered in this study consists of three modules: analysis, optimization, and control. The analysis module is used to evaluate the objective functions with a one-dimensional single channel model and the Romberg integration method. It obtains new design variables from the control module, produces the CO cumulative emissions and the integral value of a catalyst distribution function over the monolith volume, and provides objective function values to the control module. The optimal design variables for minimizing the objective functions are determined by the optimization module using a micro genetic algorithm. The control module manages the optimal design process that mainly takes place in both the analysis and optimization modules.