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Wavelet-Based Identification for Spinning Projectile with Gasodynamic Control Aerodynamic Coefficients Determination

Identification of a spinning projectile controlled with gasodynamic engines is shown in this paper. A missile model with a measurement inertial unit was developed from Newton’s law of motion and its aerodynamic coefficients were identified. This was achieved by applying the maximum likelihood princi...

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Detalles Bibliográficos
Autores principales: Lichota, Piotr, Jacewicz, Mariusz, Głębocki, Robert, Miedziński, Dariusz
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9185651/
https://www.ncbi.nlm.nih.gov/pubmed/35684712
http://dx.doi.org/10.3390/s22114090

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