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Two-manoeuvers transfers between LEOs and Lissajous orbits in the Earth-Moon system

Autor
Masdemont, J.J.; Gomez Muntané, Gerard; Alessi, E. M.
Tipus d'activitat
Article en revista
Revista
Advances in space research
Data de publicació
2010
Volum
45
Pàgina inicial
1276
Pàgina final
1291
DOI
https://doi.org/10.1016/j.asr.2009.12.010 Obrir en finestra nova
Repositori
http://hdl.handle.net/2117/7405 Obrir en finestra nova
URL
http://adsabs.harvard.edu/abs/2010AdSpR..45.1276A Obrir en finestra nova
Resum
The purpose of this work is to compute transfer trajectories from a given Low Earth Orbit (LEO) to a nominal Lissajous quasi-periodic orbit either around the point L1 or the point L2 in the Earth–Moon system. This is achieved by adopting the Circular Restricted Three-Body Problem (CR3BP) as force model and applying the tools of Dynamical Systems Theory. It is known that the CR3BP admits five equilibrium points, also called Lagrangian points, and a first integral of motion, the Jacobi integral....
Citació
Masdemont, J.J.; Gómez, G.; Alessi, E. M. Two-manoeuvers transfers between LEOs and Lissajous orbits in the Earth-Moon system. "Advances in space research", 2010, vol. 45, p. 1276-1291.
Grup de recerca
SD - Sistemes Dinàmics de la UPC

Participants