Modal parameters of spacecraft structures are important indicators
of their dynamic characteristics which can be used for vibration
reduction and control. In the present research modal parameters of
a rocket are identified by using continuous wavelet transformation.
The advantages of the wavelet transformation for the modal
parameters identification over other methods is study. Through
finite element method transient dynamic response of a system is
determined then continuous wavelet transformation is applied to
find the modal parameters like modal frequency, mode shapes and
damping ratio.
General
Is the information for this product incomplete, wrong or inappropriate?
Let us know about it.
Does this product have an incorrect or missing image?
Send us a new image.
Is this product missing categories?
Add more categories.
Review This Product
No reviews yet - be the first to create one!