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Rigid body mode identification of the PAH-2 helicopter using the eigensystem realization algorithmThe rigid body modes of the PAH-2 'Tiger' helicopter were identified using the Eigensystem Realization Algorithm (ERA). This work complements ground vibration tests performed using DLR's traditional phase resonance technique and the ISSPA (Identification of Structural System Parameters) method. Rigid body modal parameters are important for ground resonance prediction. Time-domain data for ERA were obtained by inverse Fourier transformation of frequency response functions measured with stepped-sine excitation. Mode purity (based on the Phase Resonance Criterion) was generally equal to or greater than corresponding results obtained in the ground vibration tests. All identified natural frequencies and mode shapes correlate well with corresponding ground vibration test results. The modal identification approach discussed in this report has become increasingly attractive in recent years due to the steadily declining cost and increased performance of scientific computers. As illustrated in this application, modern time-domain methods can be successfully applied to data acquired using DLR's existing test equipment. Some suggestions are made for future applications of time domain modal identification in this manner.
Document ID
19930002356
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Schenk, Axel
(Deutsche Forschungsanstalt fuer Luft- und Raumfahrt Goettingen, Germany)
Pappa, Richard S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
DLR-IB-232-91/J07
NAS 1.15:107690
NASA-TM-107690
Report Number: DLR-IB-232-91/J07
Report Number: NAS 1.15:107690
Report Number: NASA-TM-107690
Accession Number
93N11544
Funding Number(s)
PROJECT: RTOP 590-14-61-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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