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Recursive identification and tracking of parameters for linear and nonlinear multivariable systemsThe problem of identifying constant and variable parameters in multi-input, multi-output, linear and nonlinear systems is considered, using the maximum likelihood approach. An iterative algorithm, leading to recursive identification and tracking of the unknown parameters and the noise covariance matrix, is developed. Agile tracking, and accurate and unbiased identified parameters are obtained. Necessary conditions for a globally, asymptotically stable identification process are provided; the conditions proved to be useful and efficient. Among different cases studied, the stability derivatives of an aircraft were identified and some of the results are shown as examples.
Document ID
19750017888
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Sidar, M.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1975
Subject Category
Aircraft Stability And Control
Report/Patent Number
A-6115
NASA-TM-X-62446
Report Number: A-6115
Report Number: NASA-TM-X-62446
Accession Number
75N25960
Funding Number(s)
PROJECT: RTOP 505-07-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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