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Non-intrusive parameter identification procedure user's guideWritten in standard FORTRAN, NAS is capable of identifying linear as well as nonlinear relations between input and output parameters; the only restriction is that the input/output relation be linear with respect to the unknown coefficients of the estimation equations. The output of the identification algorithm can be specified to be in either the time domain (i.e., the estimation equation coefficients) or in the frequency domain (i.e., a frequency response of the estimation equation). The frame length ("window") over which the identification procedure is to take place can be specified to be any portion of the input time history, thereby allowing the freedom to start and stop the identification procedure within a time history. There also is an option which allows a sliding window, which gives a moving average over the time history. The NAS software also includes the ability to identify several assumed solutions simultaneously for the same or different input data.
Document ID
19830015047
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hanson, G. D.
(Systems Technology, Inc. Mountain View, CA, United States)
Jewell, W. F.
(Systems Technology, Inc. Mountain View, CA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1983
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-170398
TR-1188-1
NAS 1.26:170398
Accession Number
83N23318
Funding Number(s)
PROJECT: RTOP 505-31-21
CONTRACT_GRANT: NAS4-2941
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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