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Hybrid evolutionary algorithm with Hermite radial basis function interpolants for computationally expensive adjoint solvers

机译:具有Hermite径向基函数插值的混合进化算法用于计算昂贵的伴随解算器

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In this paper, we present an evolutionary algorithm hybridized with a gradient-based optimization technique in the spirit of Lamarckian learning for efficient design optimization. In order to expedite gradient search, we employ local surrogate models that approximate the outputs of a computationally expensive Euler solver. Our focus is on the case when an adjoint Euler solver is available for efficiently computing the sensitivities of the outputs with respect to the design variables. We propose the idea of using Hermite interpolation to construct gradient-enhanced radial basis function networks that incorporate sensitivity data provided by the adjoint Euler solver. Further, we conduct local search using a trust-region framework that interleaves gradient-enhanced surrogate models with the computationally expensive adjoint Euler solver. This ensures that the present hybrid evolutionary algorithm inherits the convergence properties of the classical trust-region approach. We present numerical results for airfoil aerodynamic design optimization problems to show that the proposed algorithm converges to good designs on a limited computational budget.
机译:在本文中,我们本着Lamarckian学习的精神,提出了一种与基于梯度的优化技术混合的进化算法,以进行有效的设计优化。为了加快梯度搜索,我们采用了局部代理模型来近似计算上昂贵的Euler求解器的输出。我们的重点是当有辅助的Euler求解器可用于有效地计算输出相对于设计变量的灵敏度时的情况。我们提出了使用Hermite插值来构造梯度增强的径向基函数网络的思想,该网络合并了由伴随的Euler求解器提供的灵敏度数据。此外,我们使用信任区域框架进行局部搜索,该框架将梯度增强的替代模型与计算量大的伴随欧拉求解器交织在一起。这确保了本发明的混合进化算法继承了经典信任区域方法的收敛性。我们给出了机翼空气动力学设计优化问题的数值结果,以表明所提出的算法在有限的计算预算下收敛到良好的设计。

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