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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>","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.","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>.","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>","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>.","short":"M. Tantardini, E. Fantino, Y. Ren, P. Pergola, G. Gómez, J.J. Masdemont, Celestial Mechanics and Dynamical Astronomy (2010) 215–232.","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} }"},"year":"2010","publication_identifier":{"issn":["0923-2958","1572-9478"]},"publication_status":"published","language":[{"iso":"eng"}],"department":[{"_id":"101"}],"user_id":"15701","_id":"16673","status":"public","publication":"Celestial Mechanics and Dynamical Astronomy","type":"journal_article"},{"date_updated":"2022-01-06T06:52:52Z","author":[{"first_name":"Michael","last_name":"Dellnitz","full_name":"Dellnitz, Michael"},{"first_name":"Sina","full_name":"Ober-Blöbaum, Sina","last_name":"Ober-Blöbaum"},{"last_name":"Post","full_name":"Post, Marcus","first_name":"Marcus"},{"first_name":"Oliver","last_name":"Schütze","full_name":"Schütze, Oliver"},{"last_name":"Thiere","full_name":"Thiere, Bianca","first_name":"Bianca"}],"date_created":"2020-04-16T05:05:17Z","title":"A multi-objective approach to the design of low thrust space trajectories using optimal control","doi":"10.1007/s10569-009-9229-y","publication_identifier":{"issn":["0923-2958","1572-9478"]},"publication_status":"published","year":"2009","page":"33-59","citation":{"ieee":"M. Dellnitz, S. Ober-Blöbaum, M. Post, O. Schütze, and B. Thiere, “A multi-objective approach to the design of low thrust space trajectories using optimal control,” <i>Celestial Mechanics and Dynamical Astronomy</i>, pp. 33–59, 2009.","chicago":"Dellnitz, Michael, Sina Ober-Blöbaum, Marcus Post, Oliver Schütze, and Bianca Thiere. “A Multi-Objective Approach to the Design of Low Thrust Space Trajectories Using Optimal Control.” <i>Celestial Mechanics and Dynamical Astronomy</i>, 2009, 33–59. <a href=\"https://doi.org/10.1007/s10569-009-9229-y\">https://doi.org/10.1007/s10569-009-9229-y</a>.","ama":"Dellnitz M, Ober-Blöbaum S, Post M, Schütze O, Thiere B. A multi-objective approach to the design of low thrust space trajectories using optimal control. <i>Celestial Mechanics and Dynamical Astronomy</i>. 2009:33-59. doi:<a href=\"https://doi.org/10.1007/s10569-009-9229-y\">10.1007/s10569-009-9229-y</a>","bibtex":"@article{Dellnitz_Ober-Blöbaum_Post_Schütze_Thiere_2009, title={A multi-objective approach to the design of low thrust space trajectories using optimal control}, DOI={<a href=\"https://doi.org/10.1007/s10569-009-9229-y\">10.1007/s10569-009-9229-y</a>}, journal={Celestial Mechanics and Dynamical Astronomy}, author={Dellnitz, Michael and Ober-Blöbaum, Sina and Post, Marcus and Schütze, Oliver and Thiere, Bianca}, year={2009}, pages={33–59} }","mla":"Dellnitz, Michael, et al. “A Multi-Objective Approach to the Design of Low Thrust Space Trajectories Using Optimal Control.” <i>Celestial Mechanics and Dynamical Astronomy</i>, 2009, pp. 33–59, doi:<a href=\"https://doi.org/10.1007/s10569-009-9229-y\">10.1007/s10569-009-9229-y</a>.","short":"M. 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On target for Venus – set oriented computation of energy efficient low thrust trajectories. <i>Celestial Mechanics and Dynamical Astronomy</i>, 357–370. <a href=\"https://doi.org/10.1007/s10569-006-9008-y\">https://doi.org/10.1007/s10569-006-9008-y</a>","short":"M. Dellnitz, O. Junge, M. Post, B. 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