Study of Model Uncertainties Influence on the Impact Point Dispersion for a Gasodynamicaly Controlled Projectile

The article presents the analysis of the impact point dispersion reduction using lateral correction thrusters. Two types of control algorithms are used and four sources of uncertainties are taken into account: aerodynamic parameters, thrust curve, initial conditions and IMU errors. The Monte Carlo a...

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Detalles Bibliográficos
Autores principales: Jacewicz, Mariusz, Lichota, Piotr, Miedziński, Dariusz, Głębocki, Robert
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9099792/
https://www.ncbi.nlm.nih.gov/pubmed/35590947
http://dx.doi.org/10.3390/s22093257

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9099792/
https://www.ncbi.nlm.nih.gov/pubmed/35590947
http://dx.doi.org/10.3390/s22093257

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