Frequency-domain application of an input-error method to estimate aircraft longitudinal parameters

DOI10.1080/00207728508926750zbMath0568.93059OpenAlexW2044563052MaRDI QIDQ3686596

S. C. Raisinghani

Publication date: 1985

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

Full work available at URL: https://doi.org/10.1080/00207728508926750

zbMATH Keywords

frequency domaininput-error methodlongitudinal stabilitysimulated flight data

Mathematics Subject Classification ID

Estimation and detection in stochastic control theory (93E10) Linear systems in control theory (93C05) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Identification in stochastic control theory (93E12) Model systems in control theory (93C99)

Cites Work

• Command and stability systems for aircraft: A new digital adaptive approach
• System identification. A survey
• Aircraft parameter identification by Gauss-Newton minimization technique using flight test data
• Parameter estimation by an input-error method in frequency domain
• Aircraft parameter identification by the Gauss-Newton method in the frequency domain
• Unnamed Item

This page was built for publication: Frequency-domain application of an input-error method to estimate aircraft longitudinal parameters