Identification of Modal Parameters of a Rocket

Identification of Modal Parameters of a Rocket

by Muhammad Kashif, Zeeshan Azmat, Muhammad Asif
     
 

ISBN-10: 3838351258

ISBN-13: 9783838351254

Pub. Date: 06/29/2010

Publisher: AV Akademikerverlag GmbH & Co. KG.

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…  See more details below

Overview

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.

Product Details

ISBN-13:
9783838351254
Publisher:
AV Akademikerverlag GmbH & Co. KG.
Publication date:
06/29/2010
Pages:
80
Product dimensions:
6.00(w) x 9.00(h) x 0.19(d)

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