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Modal Parameter Identification of a Spacecraft Launcher Fairing Half Shell Model.

Füllekrug, U. and Cooper, J.E. (1) (1991) Modal Parameter Identification of a Spacecraft Launcher Fairing Half Shell Model. 9th Int. Modal Analysis Conf., April 15-18, 1991, Florence, Italy..

Full text not available from this repository.

Abstract

Impulse response data from the test of a payload fairing half shell model is analysed using six time domain system identification algorithms; Polyreference. Double Least Squares, Total Least Squares, Ibrahim Time Domain, Eigensystem Realization Algorithm and Smith Least Squares. The identified parameters obtained using each of the techniques are in good agreement with each other.

Item URL in elib:https://elib.dlr.de/39446/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1991, pages=7,
Title:Modal Parameter Identification of a Spacecraft Launcher Fairing Half Shell Model.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Füllekrug, U.UNSPECIFIEDUNSPECIFIED
Cooper, J.E. (1)UNSPECIFIEDUNSPECIFIED
Date:1991
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Structural Dynamics, System Identification, Time Domain Methods.
Event Title:9th Int. Modal Analysis Conf., April 15-18, 1991, Florence, Italy.
HGF - Research field:UNSPECIFIED
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:no assignment
DLR - Research theme (Project):UNSPECIFIED
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 10:43

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