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• W3204332256 abstract "No AccessEngineering NotesDelta-V Earth-Gravity-Assist Trajectories with Hybrid Solar Electric–Photonic PropulsionYuki Takao and Toshihiro ChujoYuki Takao https://orcid.org/0000-0003-1857-6449Japan Aerospace Exploration Agency, Kanagawa 252-5210, Japan*Postdoctoral Researcher, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Chuo, Sagamihara. Member AIAA.Search for more papers by this author and Toshihiro ChujoTokyo Institute of Technology, Tokyo 152-8550, Japan†Assistant Professor, Department of Mechanical Engineering, 2-12-1 Ookayama, Meguro. Member AIAA.Search for more papers by this authorPublished Online:7 Oct 2021https://doi.org/10.2514/1.G006136SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Battin R. 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Google Scholar[27] Takao Y., Mori O., Matsushita M. and Sugihara A. K., “Solar Electric Propulsion by a Solar Power Sail for Small Spacecraft Missions to the Outer Solar System,” Acta Astronautica, Vol. 181, April 2021, pp. 362–376. https://doi.org/10.1016/j.actaastro.2021.01.020 CrossrefGoogle Scholar[28] Meng Y., Zhang H. and Gao Y., “Low-Thrust Minimum-Fuel Trajectory Optimization Using Multiple Shooting Augmented by Analytical Derivatives,” Journal of Guidance, Control, and Dynamics, Vol. 42, No. 3, 2019, pp. 662–677. https://doi.org/10.2514/1.G003473 LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Volume 45, Number 1January 2022 CrossmarkInformationCopyright © 2021 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAsteroidsAstronomyCelestial Coordinate SystemCelestial MechanicsPlanetary Science and ExplorationPlanetsSolar PhysicsSpace AgenciesSpace MissionsSpace Science and Technology KeywordsEarthSolar Electric PropulsionGravity Assist TrajectoriesHybrid PropulsionPontryagin's Maximum PrincipleFuel ConsumptionDeep Space ManeuverSynchronous OrbitSpacecraft DesignOrbital PeriodAcknowledgmentThis work was supported by Grants-in-Aid for Scientific Research (20 J01938) from the Japan Society for the Promotion of Science.PDF Received19 April 2021Accepted28 August 2021Published online7 October 2021" @default.
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