Coupled Attitude-Orbit Dynamics and Control for an Electric Sail in a Heliocentric Transfer Mission

The paper discusses the coupled attitude-orbit dynamics and control of an electric-sail-based spacecraft in a heliocentric transfer mission. The mathematical model characterizing the propulsive thrust is first described as a function of the orbital radius and the sail angle. Since the solar wind dyn...

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Detalles Bibliográficos
Autores principales: Huo, Mingying, Zhao, Jun, Xie, Shaobiao, Qi, Naiming
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Public Library of Science 2015
Materias:
Research Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4423971/
https://www.ncbi.nlm.nih.gov/pubmed/25950179
http://dx.doi.org/10.1371/journal.pone.0125901

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4423971/
https://www.ncbi.nlm.nih.gov/pubmed/25950179
http://dx.doi.org/10.1371/journal.pone.0125901

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