Applying the perturbative integral in aeromaneuvers around Mars to calculate the cost

The perturbative integral method was applied to quantify the contribution of external forces during a specific interval of time in trajectories of spacecraft around asteroids and under the Luni-solar influence. However, this method has not been used to quantify the contributions of drag in aerocaptu...

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Detalles Bibliográficos
Autores principales: Piñeros, Jhonathan O. Murcia, de Almeida Prado, Antônio F. Bertachini, dos Santos, Walter Abrahão, de Moraes, Rodolpho Vilhena
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Nature Publishing Group UK 2022
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8943136/
https://www.ncbi.nlm.nih.gov/pubmed/35322088
http://dx.doi.org/10.1038/s41598-022-08830-9

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8943136/
https://www.ncbi.nlm.nih.gov/pubmed/35322088
http://dx.doi.org/10.1038/s41598-022-08830-9

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