Optimal Trajectories for Planetary Pole-Sitter Missions
2016; American Institute of Aeronautics and Astronautics; Volume: 39; Issue: 10 Linguagem: Inglês
10.2514/1.g000465
ISSN1533-3884
AutoresMike Walmsley, Jeannette Heiligers, Matteo Ceriotti, Colin R. McInnes,
Tópico(s)Space Satellite Systems and Control
ResumoNo AccessEngineering NoteOptimal Trajectories for Planetary Pole-Sitter MissionsMike Walmsley, Jeannette Heiligers, Matteo Ceriotti and Colin McInnesMike WalmsleyUniversity of Edinburgh, Edinburgh, Scotland EH9 3FD, United Kingdom, Jeannette HeiligersDelft University of Technology, 2629 HS Delft, The Netherlands, Matteo CeriottiUniversity of Glasgow, Glasgow, Scotland G12 8QQ, United Kingdom and Colin McInnesUniversity of Glasgow, Glasgow, Scotland G12 8QQ, United KingdomPublished Online:5 Jul 2016https://doi.org/10.2514/1.G000465SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Driver J. M., "Analysis of an Arctic Polesitter," Journal of Spacecraft and Rockets, Vol. 17, No. 3, 1980, pp. 263–269. doi:https://doi.org/10.2514/3.57736 LinkGoogle Scholar[2] Heiligers J., Ceriotti M., McInnes C. R. and Biggs J. D., "Mission Analysis and Systems Design of a Near-Term and Far-Term Pole-Sitter Mission," Acta Astronautica, Vol. 94, No. 1, Jan. 2014, pp. 455–469. doi: 10.1016/j.actaastro.2012.12.015 CrossrefGoogle Scholar[3] Ceriotti M., Heiligers J. and McInnes C., "Trajectory and Spacecraft Design for a Pole-Sitter Mission," Journal of Spacecraft and Rockets, Vol. 51, No. 1, Jan. 2013, pp. 311–326. doi:https://doi.org/10.2514/1.A32477 LinkGoogle Scholar[4] McInnes C. R., Solar Sailing: Technology, Dynamics and Mission Applications, Springer Praxis Books, Berlin, 2004, pp. 32–40. Google Scholar[5] Mori O., Sawada H., Funase R., Morimoto M., Endo T., Yamamoto T., Tsuda Y., Kawakatsu Y., Kawaguchi J., Miyazaki Y. and Shirasawa Y., "First Solar Power Sail Demonstration by IKAROS," Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol. 8, No. ists27, 2010, pp. 425–431. doi: 10.2322/tastj.8.To_4_25 CrossrefGoogle Scholar[6] Johnson L., Whorton M., Heaton A., Pinson R., Laue G. and Adams C., "NanoSail-D: A Solar Sail Demonstration Mission," Acta Astronautica, Vol. 68, Nos. 5–6, 2011, pp. 571–575. doi:https://doi.org/10.1016/j.actaastro.2010.02.008 CrossrefGoogle Scholar[7] Biddy C. and Svitek T., "LightSail-1 Solar Sail Design and Qualification," Proceedings of the 41st Aerospace Mechanisms Symposium, Jet Propulsion Lab., National Aeronautics and Space Administration, Pasadena, CA, 2012, pp. 451–463, http://hdl.handle.net/2014/42161. Google Scholar[8] Ceriotti M. and McInnes C. R., "Generation of Optimal Trajectories for Earth Hybrid Pole Sitters," Journal of Guidance, Control, and Dynamics, Vol. 34, No. 3, May 2011, pp. 847–859. doi:https://doi.org/10.2514/1.50935 LinkGoogle Scholar[9] Walmsley M., "Trajectory Design for Planetary Polesitter Missions," 65th International Astronautical Congress, International Astronautical Federation IAC-15-E2.2.7, Jerusalem, Israel, 2015. Google Scholar[10] McKay R., Macdonald M., Bosquillon de Frescheville F., Vasile M., McInnes C. and Biggs J., "Non-Keplerian Orbits Using Low Thrust, High ISP Propulsion Systems," 60th International Astronautical Congress, International Astronautical Federation IAC-09-C1.2.8, Daejeon, Korea, 2009. Google Scholar[11] Schubert G., Covey C., Del Genio A., Elson L. S., Apt J., Kliore A. J., Keating G., Seiff A. and Young R. E., "Structure and Circulation of the Venus Atmosphere," Journal of Geophysical Research, Vol. 85, No. A13, 1980, pp. 8007–8025. doi:https://doi.org/10.1029/JA085iA13p08007 CrossrefGoogle Scholar[12] Dachwald B., Mengali G., Quarta A. A. and Macdonald M., "Parametric Model and Optimal Control of Solar Sails with Optical Degradation," Journal of Guidance, Control, and Dynamics, Vol. 29, No. 5, 2006, pp. 1170–1178. doi:https://doi.org/10.2514/1.20313 LinkGoogle Scholar[13] Rao A., "A Survey of Numerical Methods for Optimal Control," Advances in the Astronautical Sciences, Vol. 135, AAS Paper 09-334, 2009, pp. 497–528. Google Scholar Previous article
Referência(s)