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Galileo spacecraft modal identification using an eigensystem realization algorithmA modal parameter identification technique referred to as the Eigensystem Realization Algorithm (ERA) was applied to free-response measurements from the Galileo spacecraft modal survey test. The data were recorded following single-point random excitation of the structure. This work is one phase in a research project coordinated by the Jet Propulsion Laboratory to compare the performance of various contemporary identification techniques using Galileo data. Principal emphasis is placed on estimating the accuracy of the ERA-identified modal parameters. Various accuracy indicators, such as Modal Amplitude Coherence and Modal Phase Collinearity, are discussed. More than 20 modes of the spacecraft were identified, demonstrating the ability of the ERA method to determine the dynamics of such complex structures using only a few seconds of test data.
Document ID
19840048966
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pappa, R. S.
(NASA Langley Research Center Hampton, VA, United States)
Juang, J.-N.
(NASA Langley Research Center Structures and Dynamics Div., Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
AIAA PAPER 84-1070
Report Number: AIAA PAPER 84-1070
Accession Number
84A31753
Distribution Limits
Public
Copyright
Other

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