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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...
| Autores principales: | , , , , , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
Frontiers Media S.A.
2023
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| Materias: | |
| 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 |