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• W2055016892 abstract "No AccessEngineering NoteOrbital Motions of a Solar Sail Around the L2 Earth–Moon Libration PointShengping Gong, Junfeng Li and Jules SimoShengping GongSchool of Aerospace, Tsinghua University, 100084 Beijing, People’s Republic of China*Associate Professor, School of Aerospace; .Search for more papers by this author, Junfeng LiSchool of Aerospace, Tsinghua University, 100084 Beijing, People’s Republic of China†Professor, School of Aerospace; .Search for more papers by this author and Jules SimoDepartment of Mechanical Engineering, University of Strathclyde, Glasgow, Scotland G1 1XJ, United Kingdom‡Academic Visitor, Advanced Space Concepts Laboratory, Department of Mechanical Engineering; .Search for more papers by this authorPublished Online:25 Jun 2014https://doi.org/10.2514/1.G000063SectionsView Full TextPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] McInnes C. R., McDonald A. J., Simmons J. F. L. and MacDonald E. W., “Solar Sail Parking in Restricted Three-Body Systems,” Journal of Guidance, Control, and Dynamics, Vol. 17, No. 2, 1994, pp. 399–406. doi:https://doi.org/10.2514/3.21211 JGCDDT 0162-3192 LinkGoogle Scholar[2] Baoyin H. and McInnes C., “Solar Sail Halo Orbits at the Sun–Earth Artificial L1 Point,” Celestial Mechanics and Dynamical Astronomy, Vol. 94, No. 2, 2006, pp. 155–171. doi:https://doi.org/10.1007/s10569-005-4626-3 CrossrefGoogle Scholar[3] Baoyin H. and McInnes C. R., “Solar Sail Orbits at Artificial Sun–Earth Libration Points,” Journal of Guidance, Control, and Dynamics, Vol. 28, No. 6, 2005, pp. 1328–1330. doi:https://doi.org/10.2514/1.14598 JGCDDT 0162-3192 LinkGoogle Scholar[4] Waters T. and McInnes C., “Periodic Orbits Above the Ecliptic in the Solar-Sail Restricted Three-Body Problem,” Journal of Guidance, Control, and Dynamics, Vol. 30, No. 3, 2007, pp. 687–693. doi:https://doi.org/10.2514/1.26232 JGCDDT 0162-3192 LinkGoogle Scholar[5] Farquhar R. and Kamel A., “Quasi-Periodic Orbits About the Translunar Libration Point,” Celestial Mechanics, Vol. 7, No. 4, 1973, pp. 458–473. doi:https://doi.org/10.1007/BF01227511 CLMCAV 0008-8714 CrossrefGoogle Scholar[6] Howell K. and Marchand B., “Natural and Non-Natural Spacecraft Formations near L1 and L2 Libration Points in the Sun–Earth/Moon Ephemerics System,” Dynamical Systems: An International Journal, Vol. 20, No. 1, 2005, pp. 149–173. doi:https://doi.org/10.1080/1468936042000298224 CrossrefGoogle Scholar[7] Grebow D., Ozimek M. and Howell K., “Multi-Body Orbit Architectures for Lunar South Pole Coverage,” Advances in the Astronautical Sciences, Vol. 124, No. 2, 2006, pp. 1285–1307. ADASA9 0065-3438 Google Scholar[8] Simo J. and McInnes C. R., “Displaced Solar Sail Orbits: Dynamics and Applications,” Advances in the Astronautical Sciences, Vol. 136, 2010, pp. 1803–1816. ADASA9 0065-3438 Google Scholar[9] Simo J. and McInnes C. R., “Asymptotic Analysis of Displaced Lunar Orbits,” Journal of Guidance, Control, and Dynamics, Vol. 32, No. 5, 2009, pp. 1666–1671. doi:https://doi.org/10.2514/1.43703 JGCDDT 0162-3192 LinkGoogle Scholar[10] Simo J. and McInnes C. R., “Designing Displaced Lunar Orbits Using Low-Thrust Propulsion,” Journal of Guidance, Control, and Dynamics, Vol. 33, No. 1, 2010, pp. 259–265. doi:https://doi.org/10.2514/1.45305 JGCDDT 0162-3192 LinkGoogle Scholar[11] Tsuda Y., Mori O., Funase R., Sawada H., Yamamoto T., Saiki T., Endo T. and Kawaguchi J., “Flight Status of IKAROS Deep Space Solar Sail Demonstrator,” Acta Astronautica, Vol. 69, Nos. 9–10, 2011, pp. 833–840. doi:https://doi.org/10.1016/j.actaastro.2011.06.005 AASTCF 0094-5765 CrossrefGoogle Scholar[12] Mimasu Y., Yamaguchi T., Matsumoto M., Nakamiya M., Funase R. and Kawaguchi J., “Spinning Solar Sail Orbit Steering via Spin Rate Control,” Advances in Space Research, Vol. 48, No. 11, 2011, pp. 1810–1821. doi:https://doi.org/10.1016/j.asr.2011.08.030 ASRSDW 0273-1177 CrossrefGoogle Scholar[13] McInnes C. R., “Solar Sail Trajectories at the Lunar L2 Lagrange Point,” Journal of Spacecraft and Rockets, Vol. 30, No. 6, 1993, pp. 782–784. doi:https://doi.org/10.2514/3.26393 JSCRAG 0022-4650 LinkGoogle Scholar[14] Jovan D., Sai-Ming L. and Raman K., “Robust Adaptive Variable Structure Control of Spacecraft Under Control Input Saturation,” Journal of Guidance, Control, and Dynamics, Vol. 24, No. 1, 2001, pp. 14–22. doi:https://doi.org/10.2514/2.4704 JGCDDT 0162-3192 LinkGoogle Scholar Previous article Next article" @default.
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