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Likelihood estimation for distributed parameter models for NASA Mini-MAST trussA maximum likelihood estimation for distributed parameter models of large flexible structures was formulated. Distributed parameter models involve far fewer unknown parameters than independent modal characteristics or finite element models. The closed form solutions for the partial differential equations with corresponding boundary conditions were derived. The closed-form expressions of sensitivity functions led to highly efficient algorithms for analyzing ground or on-orbit test results. For an illustration of this approach, experimental data of the NASA Mini-MAST truss was used. The estimations of modal properties involve lateral bending modes and torsional modes. The results show that distributed parameter models are promising in the parameter estimation of large flexible structures.
Document ID
19910013036
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shen, Ji-Yao
(Old Dominion Univ. Norfolk, VA., United States)
Huang, Jen-Kuang
(Old Dominion Univ. Norfolk, VA., United States)
Taylor, Lawrence W., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1991
Publication Information
Publication: Fourth NASA Workshop on Computational Control of Flexible Aerospace Systems, Part 2
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91N22349
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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