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An eigensystem realization algorithm for modal parameter identification and model reductionA method called the eigensystem realization algorithm is developed for modal parameter identification and model reduction of dynamic systems from test data. A new approach is introduced in conjunction with the singular-value decomposition technique to derive the basic formulation of minimum order realization which is an extended version of the Ho-Kalman algorithm. The basic formulation is then transformed into modal space for modal parameter identification. Two accuracy indicators are developed to quantitatively identify the system and noise modes. For illustration of the algorithm, an example is shown using experimental data from the Galileo spacecraft.
Document ID
19850064186
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Juang, J.-N.
(NASA Langley Research Center Hampton, VA, United States)
Pappa, R. S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1985
Publication Information
Publication: Journal of Guidance, Control, and Dynamics
Volume: 8
ISSN: 0731-5090
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
ISSN: 0731-5090
Accession Number
85A46337
Distribution Limits
Public
Copyright
Other

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