Aircraft parameter identification by the Gauss-Newton method in the frequency domain

DOI10.1080/00207728508926691zbMath0568.93066OpenAlexW2039202388MaRDI QIDQ3686599

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Publication date: 1985

Published in: International Journal of Systems Science (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/00207728508926691

zbMATH Keywords

Gauss-Newton minimizationestimation of aircraft parametersfrequency-domain output-error method

Mathematics Subject Classification ID

Sampled-data control/observation systems (93C57) Identification in stochastic control theory (93E12) Dynamics of a system of particles, including celestial mechanics (70F99) Fourier and Fourier-Stieltjes transforms and other transforms of Fourier type (42A38)

Related Items (2)

Tubenet: A Special Trumpetnet for Explicit Solutions to Inverse Problems ⋮ Frequency-domain application of an input-error method to estimate aircraft longitudinal parameters

Cites Work

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• System identification. A survey
• Aircraft parameter identification by Gauss-Newton minimization technique using flight test data

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