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An adaptive learning control system for large flexible structuresThe objective of the research has been to study the design of adaptive/learning control systems for the control of large flexible structures. In the first activity an adaptive/learning control methodology for flexible space structures was investigated. The approach was based on using a modal model of the flexible structure dynamics and an output-error identification scheme to identify modal parameters. In the second activity, a least-squares identification scheme was proposed for estimating both modal parameters and modal-to-actuator and modal-to-sensor shape functions. The technique was applied to experimental data obtained from the NASA Langley beam experiment. In the third activity, a separable nonlinear least-squares approach was developed for estimating the number of excited modes, shape functions, modal parameters, and modal amplitude and velocity time functions for a flexible structure. In the final research activity, a dual-adaptive control strategy was developed for regulating the modal dynamics and identifying modal parameters of a flexible structure. A min-max approach was used for finding an input to provide modal parameter identification while not exceeding reasonable bounds on modal displacement.
Document ID
19860004827
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Thau, F. E.
(City Coll. of the City Univ. of New York NY, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:176422
NASA-CR-176422
Report Number: NAS 1.26:176422
Report Number: NASA-CR-176422
Accession Number
86N14297
Funding Number(s)
CONTRACT_GRANT: NAG1-6
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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