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结合伴随方法与梯度增强Kriging模型的高效全局优化方法-2026增刊2

郭红江,韩忠华,张科施,宋文萍   

  1. 西北工业大学
  • 收稿日期:2026-06-01 修回日期:2026-06-25 发布日期:2026-06-26
  • 通讯作者: 张科施
  • 基金资助:
    国家重点研发计划

An Efficient Global Optimization Method Combining the Adjoint Method and Gradient-Enhanced Kriging

Hong-Jiang GUO1,HAN Zhong-Hua2,Ke-Shi ZHANG1,SONG WENPING   

  • Received:2026-06-01 Revised:2026-06-25 Published:2026-06-26
  • Contact: Ke-Shi ZHANG
  • Supported by:
    National Key Research and Development Program of China

摘要: 伴随方法计算气动函数梯度的成本与维数基本无关,将其与梯度增强Kriging模型(Gradient-Enhanced Kriging, GEK)结合能够有效缓解全局优化方法面临的“维数灾难”问题。然而,现有研究仅将梯度用于改进建模精度却忽略了其在搜索导向上的潜力,导致模型训练成本大幅增加而优化效率提升有限。为此,本文提出了一种结合伴随方法和GEK代理模型的高维全局气动优化新方法,挖掘样本梯度数据中的灵敏度信息与函数下降性质,指导超参数空间降维与设计空间搜索,从而大幅提高模型训练效率和优化收敛性能。首先,提出了一种基于梯度灵敏度的超参数优化方法,利用样本梯度量化变量灵敏度,构建超参数与少量待优参数的映射关系,在保留各维度差异化特征的同时实现了大幅降维。其次,提出了一种梯度加点准则方法,利用当前最优样本的梯度信息构建Hessian矩阵和拟牛顿方向进行新样本搜索,使得局部挖掘时具有梯度类优化算法的超线性收敛速度。随后,通过高维解析函数优化算例对所提出方法进行了验证,并将其应用于ADODG Case 6机翼的多极值气动优化设计。结果表明,相较于传统基于GEK的优化方法,本文所提出的方法能够将优化时间缩短10倍以上。

关键词: 气动优化设计, 代理模型, 伴随方程, 维数灾难, GEK模型

Abstract: The integration of the adjoint method, capable of computing gradients at a cost independent of dimension, with Gradient-Enhanced Kriging (GEK) presents a promising solution to the “curse of dimensionality” in global optimization. However, existing research predominantly focuses on leveraging gradients to enhance modeling accuracy, often overlooking their potential in steering the optimi-zation trajectory. Consequently, this leads to only marginal improvements in optimization efficiency with substantial increases in training costs. To address these challenges, this paper proposes a novel high-dimensional global optimization framework combining the adjoint method and GEK. By exploiting sensitivity and function descent information inherent in sample gradients, the proposed method guides hyperparameter space reduction and design space exploration, thereby significantly enhancing model training and optimization efficiency. First, a gradient-sensitivity-based hyperparameter optimization method is introduced. This approach utilizes gradients to quantify variable sensitivities, establishing a mapping between the full set of hyperparameters and a reduced set of opti-mization parameters, achieving significant dimensionality reduction while preserving the distinct characteristics of each dimension. Second, a gradient-informed infill sampling criterion is proposed. By leveraging the gradient information to approximate the Hessian matrix and construct Quasi-Newton search directions, this method substantially improves local exploitation capabilities. The pro-posed method is validated using high-dimensional analytical benchmark functions and subsequently applied to the aerodynamic de-sign optimization of the ADODG Case 6 wing, a challenging multi-modal design problem. Results demonstrate that the proposed framework reduces the total optimization time by more than a factor of ten compared to conventional GEK-based optimization meth-od.

Key words: Aerodynamic design optimization, Surrogate model, Adjoint method, Curse of Dimensionality, Gradient-enhanced kriging

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