Spacecraft trajectories to the L3 point of the Sun–Earth three-body problem

M. Tantardini, E. Fantino, Y. Ren, P. Pergola, G. Gómez, J.J. Masdemont, Celestial Mechanics and Dynamical Astronomy (2010) 215–232.

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Journal Article | Published | English
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Celestial Mechanics and Dynamical Astronomy
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215-232
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Tantardini M, Fantino E, Ren Y, Pergola P, Gómez G, Masdemont JJ. Spacecraft trajectories to the L3 point of the Sun–Earth three-body problem. Celestial Mechanics and Dynamical Astronomy. 2010:215-232. doi:10.1007/s10569-010-9299-x
Tantardini, M., Fantino, E., Ren, Y., Pergola, P., Gómez, G., & Masdemont, J. J. (2010). Spacecraft trajectories to the L3 point of the Sun–Earth three-body problem. Celestial Mechanics and Dynamical Astronomy, 215–232. https://doi.org/10.1007/s10569-010-9299-x
@article{Tantardini_Fantino_Ren_Pergola_Gómez_Masdemont_2010, title={Spacecraft trajectories to the L3 point of the Sun–Earth three-body problem}, DOI={10.1007/s10569-010-9299-x}, journal={Celestial Mechanics and Dynamical Astronomy}, author={Tantardini, Marco and Fantino, Elena and Ren, Yuan and Pergola, Pierpaolo and Gómez, Gerard and Masdemont, Josep J.}, year={2010}, pages={215–232} }
Tantardini, Marco, Elena Fantino, Yuan Ren, Pierpaolo Pergola, Gerard Gómez, and Josep J. Masdemont. “Spacecraft Trajectories to the L3 Point of the Sun–Earth Three-Body Problem.” Celestial Mechanics and Dynamical Astronomy, 2010, 215–32. https://doi.org/10.1007/s10569-010-9299-x.
M. Tantardini, E. Fantino, Y. Ren, P. Pergola, G. Gómez, and J. J. Masdemont, “Spacecraft trajectories to the L3 point of the Sun–Earth three-body problem,” Celestial Mechanics and Dynamical Astronomy, pp. 215–232, 2010.
Tantardini, Marco, et al. “Spacecraft Trajectories to the L3 Point of the Sun–Earth Three-Body Problem.” Celestial Mechanics and Dynamical Astronomy, 2010, pp. 215–32, doi:10.1007/s10569-010-9299-x.

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