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Libration transfer design using patched elliptic three-body models and graphics processing units

Autor
Peng, H.; Bai, X.; Masdemont, J.J.; Gomez Muntané, Gerard; Xu, S.
Tipus d'activitat
Article en revista
Revista
Journal of guidance control and dynamics
Data de publicació
2017-01-01
Volum
40
Número
23
Pàgina inicial
3155
Pàgina final
3166
DOI
https://doi.org/10.2514/1.G002692 Obrir en finestra nova
Repositori
http://hdl.handle.net/2117/112591 Obrir en finestra nova
URL
https://arc.aiaa.org/doi/10.2514/1.G002692 Obrir en finestra nova
Resum
Copyright © 2016 by the American Institute of Aeronautics and Astronautics, Inc. Design of the transfer from lunar orbits to the sun-Earth libration point region by direct searching in the highfidelity ephemeris model is an accurate but time-consuming practice. A computationally efficient methodology that takes advantage of the patched elliptic restricted three-body problem model, the power of graphics processing unit parallel computing, and the programming platform of MATLAB is presented. Taki...
Citació
Peng, H., Bai, X., Masdemont, J.J., Gomez Muntané, Gerard, Xu, S. Libration transfer design using patched elliptic three-body models and graphics processing units. "Journal of guidance control and dynamics", 1 Gener 2017, vol. 40, núm. 23, p. 3155-3166.
Grup de recerca
SD - Sistemes Dinàmics de la UPC

Participants