Fixed-time regulation of spacecraft orbit and attitude coordination with optimal actuation allocation using dual quaternion

On-orbit service spacecraft with redundant actuators need to overcome orbital and attitude coupling when performing proximity maneuvers. In addition, transient/steady-state performance is required to fulfill the user-defined requirements. To these ends, this paper introduces a fixed-time tracking re...

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Detalles Bibliográficos
Autores principales: Sun, Lichao, Huang, Yanpei, Fei, Haolin, Xiao, Bo, Yeatman, Eric M., Montazeri, Allahyar, Wang, Ziwei
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Frontiers Media S.A. 2023
Materias:
Robotics and AI
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9971918/
https://www.ncbi.nlm.nih.gov/pubmed/36866152
http://dx.doi.org/10.3389/frobt.2023.1138115

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9971918/
https://www.ncbi.nlm.nih.gov/pubmed/36866152
http://dx.doi.org/10.3389/frobt.2023.1138115

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