Trajectories Derived from Periodic Orbits around the Lagrangian Point L<sub>1</sub> and Lunar Swing-Bys: Application in Transfers to Near-Earth Asteroids

Trajectories Derived from Periodic Orbits around the Lagrangian Point L<sub>1</sub> and Lunar Swing-Bys: Application in Transfers to Near-Earth Asteroids

To present a set of trajectories derived from the retrograde periodic orbits around the Lagrangian equilibrium point L<sub>1</sub>, this paper considers the Circular Restricted Three-body Problem with Earth-Moon masses (CR3BP), the Restricted Bicircular, and Full Four-Body Sun-Earth-Moon...

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Bibliographic Details
Main Authors: Rebeca S. Ribeiro, Cristiano F. de Melo, Antônio F. B. A. Prado
Format: Article
Language:English
Published: MDPI AG 2022-05-01
Series:Symmetry
Subjects:
periodic orbits
escape trajectories
lunar swing-by
near-earth asteroids
mission analysis
Online Access:https://www.mdpi.com/2073-8994/14/6/1132

Internet

https://www.mdpi.com/2073-8994/14/6/1132

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