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Application of physical parameter identification to finite-element modelsThe time domain parameter identification method described previously is applied to TRW's Large Space Structure Truss Experiment. Only control sensors and actuators are employed in the test procedure. The fit of the linear structural model to the test data is improved by more than an order of magnitude using a physically reasonable parameter set. The electro-magnetic control actuators are found to contribute significant damping due to a combination of eddy current and back electro-motive force (EMF) effects. Uncertainties in both estimated physical parameters and modal behavior variables are given.
Document ID
19870015072
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bronowicki, Allen J.
(TRW Space Technology Labs. Redondo Beach, CA, United States)
Lukich, Michael S.
(TRW Space Technology Labs. Redondo Beach, CA, United States)
Kuritz, Steven P.
(TRW Space Technology Labs. Redondo Beach, CA, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1987
Publication Information
Publication: NASA-Langley Research Center NASA(DOD Control)Structures Interaction Technology, 1986
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N24505
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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