Aircraft parameter identification by Gauss-Newton minimization technique using flight test data

DOI10.1080/00207728308926538zbMath0519.93063OpenAlexW2094921643MaRDI QIDQ3671028

Amal Kumar Adak, S. C. Raisinghani

Publication date: 1983

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

Full work available at URL: https://doi.org/10.1080/00207728308926538

zbMATH Keywords

fast Fourier transformationoutput error methodGauss-Newton minimizationflight test data

Mathematics Subject Classification ID

Newton-type methods (49M15) Estimation and detection in stochastic control theory (93E10) Identification in stochastic control theory (93E12) Stochastic stability in control theory (93E15) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (4)

Estimation of store parameters through flight testing ⋮ Parameter estimation by an input-error method in frequency domain ⋮ Frequency-domain application of an input-error method to estimate aircraft longitudinal parameters ⋮ Aircraft parameter identification by the Gauss-Newton method in the frequency domain

Cites Work

• Unnamed Item
• Unnamed Item
• Unnamed Item

This page was built for publication: Aircraft parameter identification by Gauss-Newton minimization technique using flight test data