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Common Frame Dynamics for Conically-Constrained Spacecraft Attitude Control

Attitude control subjected to pointing constraints is a requirement for most spacecraft missions carrying sensitive on-board equipment. Pointing constraints can be divided into two categories: exclusion zones that are defined for sensitive equipment such as telescopes or cameras that can be damaged...

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Detalles Bibliográficos
Autores principales: Christopher Cruz, Arnold, Bani Younes, Ahmad
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9784449/
https://www.ncbi.nlm.nih.gov/pubmed/36560371
http://dx.doi.org/10.3390/s222410003