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Spline-based distributed system identification with application to large space antennasA parameter and state estimation technique for distributed models is demonstrated through the solution of a problem generic to large space antenna system identification. Assuming the position of the reflective surface of the maypole (hoop/column) antenna to be approximated by the static two-dimensional, stretched-membrane partial differential equation with variable-stiffness coefficient functions, a spline-based approximation procedure is described that estimates the shape and stiffness functions from data set observations. For given stiffness functions, the Galerkin projection with linear spline-based functions is applied to project the distributed problem onto a finite-dimensional subspace wherein algebraic equations exist for determining a static shape (state) prediction. The stiffness functions are then parameterized by cubic splines and the parameters estimated by an output error technique. Numerical results are presented for data descriptive of a 100-m-diameter maypole antenna.
Document ID
19860054299
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Banks, H. T.
(Brown University Providence, RI, United States)
Lamm, P. K.
(Southern Methodist University Dallas, TX, United States)
Armstrong, E. S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1986
Publication Information
Publication: Journal of Guidance, Control, and Dynamics
Volume: 9
ISSN: 0731-5090
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
86A39037
Funding Number(s)
CONTRACT_GRANT: NSF MCS-82-05355
CONTRACT_GRANT: AF-AFOSR-81-0198
CONTRACT_GRANT: NAG1-258
CONTRACT_GRANT: NAS1-15810
CONTRACT_GRANT: NSF MCS-82-00883
CONTRACT_GRANT: NAS1-16394
Distribution Limits
Public
Copyright
Other

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