{"publication_status":"published","language":[{"iso":"eng"}],"page":"215-232","type":"journal_article","date_updated":"2022-01-06T06:52:54Z","publication":"Celestial Mechanics and Dynamical Astronomy","doi":"10.1007/s10569-010-9299-x","author":[{"first_name":"Marco","last_name":"Tantardini","full_name":"Tantardini, Marco"},{"first_name":"Elena","full_name":"Fantino, Elena","last_name":"Fantino"},{"last_name":"Ren","full_name":"Ren, Yuan","first_name":"Yuan"},{"first_name":"Pierpaolo","full_name":"Pergola, Pierpaolo","last_name":"Pergola"},{"first_name":"Gerard","last_name":"Gómez","full_name":"Gómez, Gerard"},{"full_name":"Masdemont, Josep J.","last_name":"Masdemont","first_name":"Josep J."}],"status":"public","year":"2010","user_id":"15701","citation":{"chicago":"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.” <i>Celestial Mechanics and Dynamical Astronomy</i>, 2010, 215–32. <a href=\"https://doi.org/10.1007/s10569-010-9299-x\">https://doi.org/10.1007/s10569-010-9299-x</a>.","short":"M. Tantardini, E. Fantino, Y. Ren, P. Pergola, G. Gómez, J.J. Masdemont, Celestial Mechanics and Dynamical Astronomy (2010) 215–232.","apa":"Tantardini, M., Fantino, E., Ren, Y., Pergola, P., Gómez, G., &#38; Masdemont, J. J. (2010). Spacecraft trajectories to the L3 point of the Sun–Earth three-body problem. <i>Celestial Mechanics and Dynamical Astronomy</i>, 215–232. <a href=\"https://doi.org/10.1007/s10569-010-9299-x\">https://doi.org/10.1007/s10569-010-9299-x</a>","ama":"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. <i>Celestial Mechanics and Dynamical Astronomy</i>. 2010:215-232. doi:<a href=\"https://doi.org/10.1007/s10569-010-9299-x\">10.1007/s10569-010-9299-x</a>","mla":"Tantardini, Marco, et al. “Spacecraft Trajectories to the L3 Point of the Sun–Earth Three-Body Problem.” <i>Celestial Mechanics and Dynamical Astronomy</i>, 2010, pp. 215–32, doi:<a href=\"https://doi.org/10.1007/s10569-010-9299-x\">10.1007/s10569-010-9299-x</a>.","bibtex":"@article{Tantardini_Fantino_Ren_Pergola_Gómez_Masdemont_2010, title={Spacecraft trajectories to the L3 point of the Sun–Earth three-body problem}, DOI={<a href=\"https://doi.org/10.1007/s10569-010-9299-x\">10.1007/s10569-010-9299-x</a>}, 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} }","ieee":"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,” <i>Celestial Mechanics and Dynamical Astronomy</i>, pp. 215–232, 2010."},"date_created":"2020-04-16T10:09:58Z","_id":"16673","title":"Spacecraft trajectories to the L3 point of the Sun–Earth three-body problem","publication_identifier":{"issn":["0923-2958","1572-9478"]},"department":[{"_id":"101"}]}