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Identification of Modal Parameters of a Rocket. Edition No. 1 - Product Image

Identification of Modal Parameters of a Rocket. Edition No. 1

  • ID: 1898823
  • March 2010
  • 80 Pages
  • VDM Publishing House

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.

Muhammad, Kashif.
Author: Muhammad Kashif B.E (Mechanical)from NED UET, Karachi, Pakistan. MS (Flight Vehicle Design) from BUAA, Beijing, China. Co-Authors: Zeeshan Azmat,Muhammad Asif B.E (Mechanical)from NED UET, Karachi, Pakistan. MS (Flight Vehicle Design) from BUAA,Beijing China
Zeeshan, Azmat.
Author: Muhammad Kashif B.E (Mechanical)from NED UET, Karachi, Pakistan. MS (Flight Vehicle Design) from BUAA, Beijing, China. Co-Authors: Zeeshan Azmat,Muhammad Asif B.E (Mechanical)from NED UET, Karachi, Pakistan. MS (Flight Vehicle Design) from BUAA,Beijing China
Muhammad, Asif.
Author: Muhammad Kashif B.E (Mechanical)from NED UET, Karachi, Pakistan. MS (Flight Vehicle Design) from BUAA, Beijing, China. Co-Authors: Zeeshan Azmat,Muhammad Asif B.E (Mechanical)from NED UET, Karachi, Pakistan. MS (Flight Vehicle Design) from BUAA,Beijing China

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