Aircraft longitudinal stability and control derivatives identification by using life cycle and Levenberg–Marquardt optimization algorithms

DOI10.1080/17415970802082773zbMath1168.76045OpenAlexW2041667572MaRDI QIDQ3612706

Marcelo Fernandes de Oliveira, Felipe Antonio Chegury Viana, Nei Salis Brasil Neto, Luiz Carlos Sandoval Góes, Benedito Carlos de Oliveira MacIel, Valder jun. Steffen

Publication date: 10 March 2009

Published in: Inverse Problems in Science and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/17415970802082773

zbMATH Keywords

system identificationparameter estimationevolutionary algorithmsoutput error methodaircraft Xavante AT-26

Mathematics Subject Classification ID

System identification (93B30) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Related Items (1)

Control augmentation design of UAVs based on deviation modification of aerodynamic focus

Cites Work

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• Parameter estimation for flight vehicles

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