Titlebook: Advances in Structural and Multidisciplinary Optimization; Proceedings of the 1 Axel Schumacher,Thomas Vietor,Kurt Maute Conference proceed

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Multicriterial Optimization of Geometrical and Structural Properties of the Basic Module of a Singlepes of modules as possible, and are not constrained by a regular tessellation of space. Their objective is to create spatial structures in given environments connecting given terminals without self-intersections and obstacle-intersections. In an ., the assembly, reconfiguration and deployment diffic

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Pseudo Expected Improvement Matrix Criteria for Parallel Expensive Multi-objective Optimization optimization (EGO) algorithm which uses a multi-objective expected improvement (EI) function as the infill criterion, is an efficient approach to solve these expensive multi-objective optimization problems. However, the state-of-the-art multi-objective EI criteria are very expensive to compute when

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Optimal Near Sun Synchronous Orbital Design of a Nadir-Pointing Cubic Satellite with the Purpose of nce requirements of subsystems are intensely coupled with the orbital parameters. Additionally, mission requirements impose some constraints on the orbit design. For instance, in Earth Observation missions, the orbit should be designed in a way that keeps its local time in an allowable range during

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Simple Intuitive Multi-objective ParalLElization of Efficient Global Optimization: SIMPLE-EGOconstructs a Kriging approximation of the cost function, and then improves this approximation by adding additional designs to the initial designs. These aditional designs are added sequentially, one by one. In a specific iteration, the design is added where the Expected Improvement (EI) acquisition

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Gaussian Process for Aerodynamic Pressures Prediction in Fast Fluid Structure Interaction Simulationan endanger the structure itself. Predicting these interactions is a time consuming but crucial task in an aircraft design process. In order to reduce the computational time surrogate reduced order models can be used in both structural and aerodynamic models. More over it is possible to avoid launch

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Metamodel-Based Multidisciplinary Design Optimization of a General Aviation Aircraft comprehensive and appropriate meta-model with acceptable accuracy to cover the entire design space is difficult and almost impossible. This paper proposed a strategy to improve the accuracy of the created meta-models using the elimination of outlier data from sampled points and re-designing the eff

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