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Minimum-fuel escape from two body sun-earth system

Autor
Colasurdo, G.; Casalino, L.; Fantino, E.
Tipus d'activitat
Article en revista
Revista
Journal of guidance control and dynamics
Data de publicació
1999
Volum
22
Número
5
Pàgina inicial
632
Pàgina final
636
DOI
https://doi.org/10.2514/2.4446 Obrir en finestra nova
Repositori
http://hdl.handle.net/2117/23186 Obrir en finestra nova
Resum
Escaping from the solar system by receiving gravity assist from the Earth is considered in this paper . A simple procedure, which neglects the eccentricity of the Earth’ s orbit and uses the two-body problem equations and the patched-conic approximation, provides near-optimal trajectories using either a single or multiple Earth  ybys. The analysis shows that the amount of propellant required to escape from the solar system decreases with the number of  ybys, but the mission time increases....
Citació
Colasurdo, G.; Casalino, L.; Fantino, E. Minimum-fuel escape from two body sun-earth system. "Journal of guidance control and dynamics", 1999, vol. 22, núm. 5, p. 632-636.
Grup de recerca
L'AIRE - Laboratori Aeronàutic i Industrial de Recerca i Estudis

Participants

  • Colasurdo, Guido  (autor)
  • Casalino, Lorenzo  (autor)
  • Fantino, Elena  (autor)