Autor/Autorin: Kashif Muhammad
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
Autor/Autorin: Azmat Zeeshan
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
Autor/Autorin: Asif Muhammad
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
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.
Über den Autor
Author: Muhamamd Asif B.E (Mechanical) from NED UET, Karachi, Pakistan. MS (Flight Vehicle Design) from BUAA, China. Recently Working in a research organization. Co-Author: Zeeshan Azmat, Muhamamd Kashif B.E (Mechanical) from NED UET, Karachi, Pakistan. MS (Flight Vehicle Design) from BUAA, China. Recently Working in a research organization.
Klappentext
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.
