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An on-line equivalent system identification scheme for adaptive controlA prime obstacle to the widespread use of adaptive control is the degradation of performance and possible instability resulting from the presence of unmodeled dynamics. The approach taken is to explicitly include the unstructured model uncertainty in the output error identification algorithm. The order of the compensator is successively increased by including identified modes. During this model building stage, heuristic rules are used to test for convergence prior to designing compensators. Additionally, the recursive identification algorithm as extended to multi-input, multi-output systems. Enhancements were also made to reduce the computational burden of an algorithm for obtaining minimal state space realizations from the inexact, multivariate transfer functions which result from the identification process. A number of potential adaptive control applications for this approach are illustrated using computer simulations. Results indicated that when speed of adaptation and plant stability are not critical, the proposed schemes converge to enhance system performance.
Document ID
19840009117
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Sliwa, S. M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-85737
NAS 1.15:85737
Accession Number
84N17185
Funding Number(s)
PROJECT: RTOP 505-34-03-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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