Generalized Linear Quadratic Control for a Full Tracking Problem in Aviation

In this paper, the full tracking problem in aircraft system identification and control is presented. Time domain output error method with maximum likelihood principle was used to perform system identification. The linear quadratic regulator (LQR)-based approach has been used for solving aviation ful...

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Detalles Bibliográficos
Autores principales: Dul, Franciszek, Lichota, Piotr, Rusowicz, Artur
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2020
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7285372/
https://www.ncbi.nlm.nih.gov/pubmed/32456081
http://dx.doi.org/10.3390/s20102955

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7285372/
https://www.ncbi.nlm.nih.gov/pubmed/32456081
http://dx.doi.org/10.3390/s20102955

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