A FE model updating method for the simulation of the assembly process of large and lightweight aeronautical structures
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We propose a model updating process to improve the quality of a finite element model (mass and stiffness parameters).

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The method is applied to highly flexible structures.

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A measurement technology used to acquire the experimental data in the absence of any information on the actual weightless and load-free structure is proposed.

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The updating method is based on the concept of error in the constitutive relation.

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The method is illustrated and validated on two examples.

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