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Station-Keeping for Periodic Orbits near Strongly Perturbed Binary Asteroid Systems

2019; American Institute of Aeronautics and Astronautics; Volume: 43; Issue: 2 Linguagem: Inglês

10.2514/1.g004638

1533-3884

Yu Shi, Yue Wang, Arun K. Misra, Shijie Xu,

Planetary Science and Exploration

No AccessEngineering NotesStation-Keeping for Periodic Orbits near Strongly Perturbed Binary Asteroid SystemsYu Shi, Yue Wang, Arun K. Misra and Shijie XuYu ShiChinese Academy of Sciences, 100094 Beijing, People’s Republic of China*Assistant Research Professor, Technology and Engineering Center for Space Utilization; .Search for more papers by this author, Yue WangBeihang University, 102206 Beijing, People’s Republic of China†Associate Professor, School of Astronautics; (Corresponding Author).Search for more papers by this author, Arun K. MisraMcGill University, Montreal, Quebec H3A 0C3, Canada‡Thomas Workman Professor, Department of Mechanical Engineering; .Search for more papers by this author and Shijie XuBeihang University, 102206 Beijing, People’s Republic of China§Professor, School of Astronautics; .Search for more papers by this authorPublished Online:16 Oct 2019https://doi.org/10.2514/1.G004638SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Ćuk M. and Nesvorný D., “Orbital Evolution of Small Binary Asteroids,” Icarus, Vol. 207, No. 2, 2010, pp. 732–743. https://doi.org/10.1016/j.icarus.2009.12.005 CrossrefGoogle Scholar[2] Jiang Y., Baoyin H. and Zhang Y., “Relative Effect of Inclinations for Moonlets in the Triple Asteroidal Systems,” Earth, Moon, and Planets, Vol. 119, Nos. 2–3, 2017, pp. 65–83. https://doi.org/10.1007/s11038-016-9500-7 CrossrefGoogle Scholar[3] Koon W. S., Marsden J. 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TopicsAerospace SciencesAsteroidsAstrodynamicsAstronauticsAstronomyCelestial MechanicsOrbital ManeuversPlanetary Science and ExplorationPlanetsSolar PhysicsSpace MissionsSpace OrbitSpace Science and Technology KeywordsAsteroidsLinear Quadratic RegulatorFeedback ControlMonte Carlo SimulationOrbit DeterminationSolar RadiationHalo OrbitPerturbed OrbitSpace MissionsEarthAcknowledgmentsThis work has been supported by the National Natural Science Foundation of China under Grants 11872007, 11432001, and 11602009; the Young Elite Scientist Sponsorship Program by China Association for Science and Technology; the Chinese Academy of Sciences under the Key Research Program (Grant No. ZDRW-KT-2019-1-0102); and the Fundamental Research Funds for the Central Universities.PDF Received6 June 2019Accepted26 September 2019Published online16 October 2019