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This paper outlines an architecture for simultaneous analysis and robustness and reliability calculations in aircraft design optimization. Robust Design Optimization and Reliability Based Design Optimization are merged into a unied formulation which streamlines the setup of optimization problems and aims at preventing foreseeable implementation issues. The code in development expands upon and, in some cases, completely rewrites a previous version of a Multidisciplinary Design Optimization tool that was solely oriented to deterministic problems.
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Paiva et al. (2010) studied this question.
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