Barrier Function Adaptive Nonsingular Terminal Sliding Mode Control Approach for Quad-Rotor Unmanned Aerial Vehicles

This paper proposes a barrier function adaptive non-singular terminal sliding mode controller for a six-degrees-of-freedom (6DoF) quad-rotor in the existence of matched disturbances. For this reason, a linear sliding surface according to the tracking error dynamics is proposed for the convergence of...

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Detalles Bibliográficos
Autores principales: Alattas, Khalid A., Mofid, Omid, Alanazi, Abdullah K., Abo-Dief, Hala M., Bartoszewicz, Andrzej, Bakouri, Mohsen, Mobayen, Saleh
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8838949/
https://www.ncbi.nlm.nih.gov/pubmed/35161656
http://dx.doi.org/10.3390/s22030909

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8838949/
https://www.ncbi.nlm.nih.gov/pubmed/35161656
http://dx.doi.org/10.3390/s22030909

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