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The numerical cases based on the simulated modal identification procedure have demonstrated that the error in the estimation of modal parameters caused by arbitrarily choosing damping model is quite small.
The beam model considered is a Timoshenko beam, which, with the use of the transfer matrix method, estimates the changes in various modal parameters caused by the shape parameters and boundary conditions of beams.
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Existence of damping in the structure causes the modal parameters to be identified as complex data.
The rotation of spacecraft flexible appendage may cause changes in modal parameters.
Therefore, the variations of these physical properties will cause changes in the modal parameters.
The modal parameters determined through the analytical model have been considered as reference for comparison.
These modal parameters were then checked using theoretical modal analysis.
The structural modal parameters can be first obtained by theoretical modal analysis (TMA) or by experimental modal analysis (EMA).
The modal parameters for decomposition and modelling can be extracted from theoretical or experimental modal analysis.
The modal parameters were numerically predicted and experimentally validated.
Modal parameters comprise natural frequencies, damping ratios, modal vectors and modal masses.
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