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Attitude Stabilization of Spacecraft in Very Low Earth Orbit by Center-Of-Mass Shifting

At very low orbital altitudes (≲450 km) the aerodynamic forces can become major attitude disturbances. Certain missions that would benefit from a very low operational altitude require stable attitudes. The use of internal shifting masses, actively shifting the location of the spacecraft center-of-ma...

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Detalles Bibliográficos
Autores principales: Virgili-Llop, Josep, Polat, Halis C., Romano, Marcello
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Frontiers Media S.A. 2019
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7805854/
https://www.ncbi.nlm.nih.gov/pubmed/33501024
http://dx.doi.org/10.3389/frobt.2019.00007