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Improved intelligent genetic algorithm applied to long-endurance airfoil optimization design

机译:改进的智能遗传算法在长寿命机翼优化设计中的应用

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摘要

This study presents a genetic algorithm (GA) with simulated annealing (SA) mutation that has been improved by including a fractional factorial design for the crossover operator and SA for the mutation operator. The proposed GA generates the chromosomes of children using an intelligent crossover process with factorial experiments, rather than exchanging the genes at random using the one-point, two-point, multi-point, or uniform crossover employed in a traditional GA. Therefore, the GA with the intelligent crossover operator is referred to as the intelligent genetic algorithm (IGA) in this article. The SA mutation was employed to replace the conventional jump mutation in order to enhance the search process and avoid individuals becoming trapped in local optima. The performance of the proposed IGA was assessed via a nonlinear multimodal function with two design variables. Four representative test cases (Sphere, Rosenbrock, Rastrigin and Griewank functions) by used the IGA with SA mutation, micro-IGA, and IGA with jump mutation to evaluate the capacity and efficiency of the proposed IGA in terms of large design variables. Computational results of the convergence history and optimal solution for the benchmarking cases indicate that the proposed IGA with SA mutation outperforms the micro-IGA and IGA with jump mutation. Two profile fittings of NACA 4415 and LS(1)-0417 Modified airfoils are also performed using the proposed IGA with SA mutation. The proposed IGA is also applied to long-endurance airfoil optimization design.
机译:这项研究提出了一种具有模拟退火(SA)突变的遗传算法(GA),该算法已得到改进,其中包括针对交叉算子的分数阶因子设计和针对突变算子的SA。拟议的遗传算法使用因子分析的智能交叉过程生成孩子的染色体,而不是使用传统遗传算法中使用的单点,两点,多点或均匀交叉随机交换基因。因此,本文将具有智能交叉算子的GA称为智能遗传算法(IGA)。为了增强搜索过程并避免个体陷入局部最优状态,使用了SA突变来代替传统的跳跃突变。通过具有两个设计变量的非线性多峰函数评估了建议的IGA的性能。四个具有代表性的测试用例(Sphere,Rosenbrock,Rastrigin和Griewank函数)通过​​使用具有SA突变的IGA,微型IGA和具有跳跃突变的IGA来评估建议的IGA在大设计变量方面的能力和效率。收敛历史的计算结果和基准案例的最佳解决方案表明,提出的具有SA突变的IGA优于具有跳跃突变的micro-IGA和IGA。使用建议的带有SA突变的IGA,还完成了NACA 4415和LS(1)-0417修改型机翼的两个轮廓拟合。提出的IGA也可应用于长寿命机翼优化设计。

著录项

  • 来源
    《Engineering Optimization》 |2009年第2期|p.137-154|共18页
  • 作者

    Jenn-Long Liu;

  • 作者单位

    Department of Information Management, National Sun Yat-Sen University, Taiwan, ROC Department of Information Management, I-Shou University, Taiwan, ROC;

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  • 正文语种 eng
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