Neuro-fuzzy system based proportional derivative gain optimized attitude control of CubeSat under LEO perturbations

Prompt attitude stabilization is more challenging in Nano CubeSat due to its minimal capacity, weight, energy, and volume-constrained architecture. Fixed gain non-adaptive classical proportional integral derivative control methodology is ineffective to provide optimal attitude stability in low earth...

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Detalles Bibliográficos
Autores principales: Shehzad, Muhammad Faisal, Asghar, Aamer Bilal, Jaffery, Mujtaba Hussain, Naveed, Khazina, Čonka, Zsolt
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Elsevier 2023
Materias:
Research Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10551572/
https://www.ncbi.nlm.nih.gov/pubmed/37810865
http://dx.doi.org/10.1016/j.heliyon.2023.e20434

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10551572/
https://www.ncbi.nlm.nih.gov/pubmed/37810865
http://dx.doi.org/10.1016/j.heliyon.2023.e20434

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