首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Assessment of Multiobjective Genetic Algorithms With Different Niching Strategies and Regression Methods for Engine Optimization and Design
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Assessment of Multiobjective Genetic Algorithms With Different Niching Strategies and Regression Methods for Engine Optimization and Design

机译:发动机优化设计的不同定位策略和回归方法的多目标遗传算法评估。

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In a previous study (Shi, Y., and Reitz, R. D., 2008, "Assessment of Optimization Methodologies to Study the Effects of Bowl Geometry, Spray Targeting and Swirl Ratio for a Heavy-Duty Diesel Engine Operated at High-Load," SAE Paper No. 2008-01-0949), nondominated sorting genetic algorithm II (NSGA II) (Deb, K., Pratap, A., Agarwal, S., and Meyarivan, T, 2002, "A Fast and Elitist Multiobjective Genetic Algorithm: NSGA-II," IEEE Trans. Evol. Comput., 6, pp. 182.197) performed better than other popular multiobjective genetic algorithms (MOGAs) in engine optimization that sought optimal combinations of the piston bowl geometry, spray targeting, and swirl ratio. NSGA II is further studied in this paper using different niching strategies that are applied to the objective space and design space, which diversify the optimal objectives and design parameters, accordingly. Convergence and diversity metrics are defined to assess the performance of NSGA II using different niching strategies. It was found that use of design niching achieved more diversified results with respect to design parameters, as expected. Regression was then conducted on the design data sets that were obtained from the optimizations with two niching strategies. Four regression methods, including K-nearest neighbors (KNs), kriging (KR), neural networks (NNs), and radial basis functions (RBFs), were compared. The results showed that the data set obtained from optimization with objective niching provided a more fitted learning space for the regression methods. KNs and KR outperformed the other two methods with respect to prediction accuracy. Furthermore, a log transformation to the objective space improved the prediction accuracy for the KN, KR, and NN methods, except the RBF method. The results indicate that it is appropriate to use a regression tool to partly replace the actual CFD evaluation tool in engine optimization designs using the genetic algorithm. This hybrid mode saves computational resources (processors) without losing optimal accuracy. A design of experiment (DoE) method (the optimal Latin hypercube method) was also used to generate a data set for the regression processes. However, the predicted results were much less reliable than the results that were learned using the dynamically increasing data sets from the NSGA II generations. Applying the dynamical learning strategy during the optimization processes allows computationally expensive CFD evaluations to be partly replaced by evaluations using the regression techniques. The present study demonstrates the feasibility of applying the hybrid mode to engine optimization problems, and the conclusions can also extend to other optimization studies (numerical or experimental) that feature time-consuming evaluations and have highly nonlinear objective spaces.
机译:在先前的研究中(Shi,Y。和Reitz,RD,2008,“优化方法的评估,以研究高负荷运行的重型柴油机的转鼓几何形状,喷射目标和涡流比的影响”,SAE论文编号2008-01-0949),非支配排序遗传算法II(NSGA II)(Deb,K.,Pratap,A.,Agarwal,S.和Meyarivan,T,2002年,“一种快速而精英的多目标遗传算法:“ NSGA-II”,“ IEEE Trans。Evol。Comput。,第6页,第182.197页)在发动机优化中的表现优于其他流行的多目标遗传算法(MOGA),该算法寻求活塞碗几何形状,喷雾目标和涡流比的最佳组合。在本文中,使用了应用于目标空间和设计空间的不同小生境策略进一步研究了NSGA II,从而使最优目标和设计参数多样化。定义了收敛和多样性指标,以使用不同的固定策略来评估NSGA II的性能。发现,如预期的那样,使用设计小生境在设计参数方面获得了更加多样化的结果。然后对通过两种小策略从优化中获得的设计数据集进行回归。比较了四种回归方法,包括K最近邻(KNs),kriging(KR),神经网络(NNs)和径向基函数(RBFs)。结果表明,通过客观定位优化获得的数据集为回归方法提供了更合适的学习空间。就预测准确性而言,KNs和KR优于其他两种方法。此外,除RBF方法外,对目标空间的对数变换提高了KN,KR和NN方法的预测精度。结果表明,使用遗传算法在发动机优化设计中使用回归工具部分替代实际的CFD评估工具是适当的。这种混合模式可节省计算资源(处理器),而不会损失最佳精度。实验(DoE)方法(最佳拉丁超立方体方法)的设计也用于生成回归过程的数据集。但是,预测结果的可靠性远不如使用从NSGA II代中动态增加的数据集获得的结果可靠。在优化过程中应用动态学习策略可以使计算量大的CFD评估部分被使用回归技术的评估所替代。本研究证明了将混合模式应用于发动机优化问题的可行性,其结论还可以扩展到具有耗时评估且具有高度非线性目标空间的其他优化研究(数值或实验)。

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