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Identification of Modal Parameters of a Rocket
Contributor(s): Kashif, Muhammad (Author), Azmat, Zeeshan (Author), Asif, Muhammad (Author)
ISBN: 3838351258     ISBN-13: 9783838351254
Publisher: LAP Lambert Academic Publishing
OUR PRICE:   $50.27  
Product Type: Paperback
Published: June 2010
Qty:
Additional Information
BISAC Categories:
- Technology & Engineering | Aeronautics & Astronautics
Physical Information: 0.19" H x 6" W x 9" (0.28 lbs) 80 pages
 
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Publisher Description:
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.