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Aerodynamic parameter estimation via Fourier modulating function techniquesParameter estimation algorithms are developed in the frequency domain for systems modeled by input/output ordinary differential equations. The approach is based on Shinbrot's method of moment functionals utilizing Fourier based modulating functions. Assuming white measurement noises for linear multivariable system models, an adaptive weighted least squares algorithm is developed which approximates a maximum likelihood estimate and cannot be biased by unknown initial or boundary conditions in the data owing to a special property attending Shinbrot-type modulating functions. Application is made to perturbation equation modeling of the longitudinal and lateral dynamics of a high performance aircraft using flight-test data. Comparative studies are included which demonstrate potential advantages of the algorithm relative to some well established techniques for parameter identification. Deterministic least squares extensions of the approach are made to the frequency transfer function identification problem for linear systems and to the parameter identification problem for a class of nonlinear-time-varying differential system models.
Document ID
19950018210
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pearson, A. E.
(Brown Univ. Providence, RI, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1995
Publication Information
Publisher: NASA
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-4654
NAS 1.26:4654
Report Number: NASA-CR-4654
Report Number: NAS 1.26:4654
Accession Number
95N24630
Funding Number(s)
PROJECT: RTOP 505-64-52-01
CONTRACT_GRANT: NAG1-1065
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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