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..

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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:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Füllekrug, U.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Cooper, J.E. (1)	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

1991

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

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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