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A new method for reliability analysis and reliability-based design optimization

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Abstract

We present a novel method for reliability-based design optimization, which is based on the approximation of the safe region in the random space by a polytope-like region. This polytope is in its turn transformed into quite a simple region by using generalized spherical coordinates. The failure probability can then be easily estimated by considering simple quadrature rules. One of the advantages of the proposed approach is that by increasing the number of vertices, we can improve arbitrarily the accuracy of the failure probability estimation. The sensitivity analysis of the failure probability is also provided. We show that the proposed approach leads to an optimization problem, where the set of optimization variables includes all the original design variables and all the parameters that control the shape of the polytope. In addition, this problem can be solved by a single iteration scheme of optimization. We illustrate the performance of the new approach by solving several examples of truss topology optimization.

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Acknowledgements

Alfredo Canelas thanks the Uruguayan Councils ANII and CSIC for the financial support.

Funding

This research was supported by CONICYT-Chile, via FONDECYT project 1160894.

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Correspondence to Alfredo Canelas.

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Appendix: Closed formula for the MPP

Appendix: Closed formula for the MPP

Since the random load is f = Fξ, and xε, then c(x,ξ) = ξFK(x)− 1Fξ. By calling M(x) = FK(x)− 1F, we have that the MPP can be found as the solution ξ to

$$\begin{array}{@{}rcl@{}} &\ &\underset{\boldsymbol{\xi}}\min \boldsymbol{\xi}^{\top} \boldsymbol{\xi} , \\ &&\text{s.t. } \boldsymbol{\xi}^{\top} \mathbf{M}(\mathbf{x}) \boldsymbol{\xi} \ge c_{0} . \end{array} $$

Note that the inequality constraint must be active at the solution (the MPP is in the failure surface), since the only possible interior solution is ξ = 0 which does not satisfy the constraint for a positive c0. Hence, let λ be the nonnegative Lagrange multiplier of the constraint at the solution. The first order optimality condition is ξλM(x)ξ = 0. The value λ = 0 is not a possible solution since it leads to ξ = 0. Hence λ > 0. Let μ = λ− 1. Then, from the optimality condition we obtain M(x)ξ = μξ. Hence ξ must be an eigenvector of M(x) of eigenvalue μ. Let v be a unit eigenvector of eigenvalue μ, i.e. M(x)v = μv with vv = 1. Then ξ = αv for certain value α. Since the constraint is active ξM(x)ξ = α2vM(x)v = α2μ = c0. Then α2 = c0/μ and ξ = αv = (c0/μ)1/2v. Since the objective function is ξξ = α2 = c0/μ, then μ must be the maximum eigenvalue of M(x).

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Canelas, A., Carrasco, M. & López, J. A new method for reliability analysis and reliability-based design optimization. Struct Multidisc Optim 59, 1655–1671 (2019). https://doi.org/10.1007/s00158-018-2151-8

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