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This study proposes a numerical modeling method to simulate the dynamic motion of highly flexible and deployable aerospace structures such as truss antennas and deployable wing aircraft. Simulation results present the advantages and accuracy of the proposed method.

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This page is a summary of: Absolute Nodal Coordinate Beam Element for Modeling Flexible and Deployable Aerospace Structures, AIAA Journal, March 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j057780.
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