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首页> 外文期刊>Journal of Advanced Mechanical Design, Systems, and Manufacturing >Development of efficient global optimization method for discontinuous optimization problems with infeasible regions using classification method
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Development of efficient global optimization method for discontinuous optimization problems with infeasible regions using classification method

机译:利用分类方法开发不可行区域不连续优化问题的高效全局优化方法

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摘要

The objective of this research is to efficiently solve discontinuous optimization problems as well as optimization problems with large infeasible regions in the design variables space. Recently, major optimization targets have been changed to more complicated ones such as topology optimization problem, discontinuous optimization problem, robust optimization problem and high dimensional optimization problem. The aim of this research is to efficiently solve the complicated optimization problems by using machine learning technologies. In aerodynamic optimization problems at supersonic flow conditions, it is confirmed that aerodynamic objective functions have discontinuity due to shock waves and it needs to treat the discontinuous functions and large infeasible regions via strong shock waves. In this research, therefore, we develop an efficient global optimization method for discontinuous optimization problems with infeasible regions using classification method (EGODISC). The developed method is compared with a Bayesian optimization method using the Matern 5/2 kernel Gaussian process regression and a genetic algorithm to verify the usefulness of the developed method. The Bayesian optimization falls into an infinite loop in its optimization process by selecting an additional sample point in the infeasible regions. On the other hand, the developed method can work well with the infeasible regions in the design variables space. It is confirmed that EGODISC can be effectively used with discontinuous aerodynamic objective functions. It is also confirmed that EGODISC can be effectively used for a shape optimization problem with large infeasible regions by the negative thickness of airfoil.
机译:这项研究的目的是有效解决不连续的优化问题以及设计变量空间中不可行区域较大的优化问题。近来,主要的优化目标已经改变为更复杂的目标,例如拓扑优化问题,不连续优化问题,鲁棒优化问题和高维优化问题。这项研究的目的是通过使用机器学习技术来有效地解决复杂的优化问题。在超声速流动条件下的空气动力学优化问题中,已确认空气动力学目标函数由于冲击波而具有不连续性,因此需要通过强冲击波来处理不连续函数和较大的不可行区域。因此,在这项研究中,我们使用分类方法(EGODISC)为不可行区域的不连续优化问题开发了一种有效的全局优化方法。将所开发的方法与使用Matern 5/2核高斯过程回归和遗传算法的贝叶斯优化方法进行比较,以验证所开发方法的有效性。通过在不可行区域中选择其他采样点,贝叶斯优化在其优化过程中陷入无限循环。另一方面,所开发的方法可以很好地解决设计变量空间中不可行的区域。可以肯定的是,EGODISC可以有效地用于不连续的空气动力学目标函数。还证实了,EGODISC可以有效地用于翼型厚度为负数的不可行区域较大的形状优化问题。

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