Results of short-period helicopter system identification using output-error and hybrid search-gradient optimization algorithm

DOI10.1155/2010/231594zbMath1205.93154OpenAlexW2054620243WikidataQ58652967 ScholiaQ58652967MaRDI QIDQ1958811

Ronaldo Vieira Cruz, Luiz Carlos Sandoval Góes

Publication date: 30 September 2010

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://eudml.org/doc/231655

zbMATH Keywords

parameter estimationidentification problemgenetic algorithm (GA)estimation of aerodynamic derivativesLevenberg-Marquardt optimization algorithmsoutput-error approach

Mathematics Subject Classification ID

Approximation methods and heuristics in mathematical programming (90C59) Application models in control theory (93C95) Estimation and detection in stochastic control theory (93E10) Identification in stochastic control theory (93E12) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (1)

Chaos-genetic algorithm for the system identification of a small unmanned helicopter

Cites Work

• Dynamic system identification. Experiment design and data analysis
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