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Solving Very Large-Scale Structural Optimization Problems

机译:解决大型结构优化问题

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摘要

Large-scale structural parametric optimization problems still impose a challenge to computer hardware. A three-step approach to reduce the run time and memory requirements is proposed. It is based on the observed sparsity of the matrix of partial derivatives in structural optimization. The approach includes a differentiation scheme to compute smaller gradient matrices in parallel and assemble them employing the chain rule, an adaptive filtering framework for an effective selection of active constraints based on numerical value and engineering knowledge and the pairing of a known sequential convex programming algorithm with a preconditioned conjugate gradient solver for the internal matrices. Software has been developed and successfully applied to the optimization of the outer wing panels of a large military transporter aircraft.
机译:大规模的结构参数优化问题仍然对计算机硬件构成了挑战。提出了一种减少运行时间和内存需求的三步方法。它基于结构优化中偏导数矩阵的稀疏性。该方法包括一个微分方案,可并行计算较小的梯度矩阵,并使用链式规则进行组装;自适应滤波框架,可基于数值和工程知识有效选择活动约束;将已知的顺序凸规划算法与用于内部矩阵的预处理共轭梯度求解器。已经开发了软件并将其成功应用于大型军用运输机的外机翼板的优化。

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