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A Review of System Identification Methods Applied to AircraftAirplane identification, equation error method, maximum likelihood method, parameter estimation in frequency domain, extended Kalman filter, aircraft equations of motion, aerodynamic model equations, criteria for the selection of a parsimonious model, and online aircraft identification are addressed.
Document ID
19830025630
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Klein, V. (Joint Inst. for Acoustics and Flight Sciences Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
August 1, 1983
Publication Information
Publication: NASA. Langley Research Center Restructurable Controls
Subject Category
Aircraft Stability And Control
Accession Number
83N33901
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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