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Nonlinear Robust Performance Analysis using Gradient-Based Optimisation - An Aeroelastic Case-Study

机译:基于梯度优化的非线性鲁棒性能分析 - 气弹性案例研究

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This paper considers the problem of computing lower bounds on the worst-case performance of nonlinear systems using gradient-based optimisation. Four different gradient-based local optimisation methods are applied to a robust performance analysis problem for a nonlinear aeroelastic system. The first method formulates the optimisation problem in the classical Euler-Lagrange setting and computes the gradient by backward integration of the resulting adjoint system. The second method also uses the Euler-Lagrange formulation, but uses complex perturbations to calculate the gradient. The third method employs Sequential Quadratic Programming, while the fourth method considered is Simultaneous Perturbation Stochastic Approximation (SPSA), which uses a stochastic approach to decide the search direction. The performance of all four methods is evaluated in terms of computational complexity, numerical accuracy, and ease of implementation, and compared with a standard industrial approach based on a gridding of the uncertain parameter space.
机译:本文考虑计算上使用基于梯度的优化非线性系统的最坏情况下的性能下界的问题。四种不同的基于梯度的局部优化方法适用于一个强大的性能分析问题的非线性气动弹性系统。第一种方法制定在经典的欧拉 - 拉格朗日设置的优化问题,并通过将得到的共轭系统的后向一体化计算梯度。第二种方法也使用欧拉 - 拉格朗日制剂,但使用复杂的扰动来计算梯度。第三种方法采用序列二次规划,而考虑的第四种方法是同步扰动随机逼近(SPSA),它使用一个随机方法来决定搜索方向。这四种方法的性能的计算复杂性,数值精度和易于实施方面进行评估,并基于不确定参数空间网格化标准工业方法相比。

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