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Energy-Saving Capture at Mars via Backward-Stable Orbits

2019; American Institute of Aeronautics and Astronautics; Volume: 42; Issue: 5 Linguagem: Inglês

10.2514/1.g004006

1533-3884

Xiangyu Li, Dong Qiao, Malcolm Macdonald,

Space Satellite Systems and Control

No AccessEngineering NotesEnergy-Saving Capture at Mars via Backward-Stable OrbitsXiangyu Li, Dong Qiao and Malcolm MacdonaldXiangyu LiBeijing Institute of Technology, 100081 Beijing, People's Republic of China, Dong QiaoBeijing Institute of Technology, 100081 Beijing, People's Republic of China and Malcolm MacdonaldUniversity of Strathclyde, Glasgow, Scotland G1 1XJ, United KingdomPublished Online:19 Feb 2019https://doi.org/10.2514/1.G004006SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Belbruno E. A. and Miller J. K., "Sun-Perturbed Earth-to-Moon Transfers with Ballistic Capture," Journal of Guidance, Control, and Dynamics, Vol. 16, No. 4, 1993, pp. 770–775. doi:https://doi.org/10.2514/3.21079 JGCODS 0731-5090 LinkGoogle Scholar[2] Chung M., Hatch S. J., Kangas J. A., Long S. M., Roncoli R. B. and Sweetser T. 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J., Yamakawa H. and Yoshikawa M., "Analysis of Capture Trajectories into Periodic Orbits About Libration Points," Journal of Guidance, Control, and Dynamics, Vol. 31, No. 5, 2008, pp. 1344–1351. doi:https://doi.org/10.2514/1.33796 JGCODS 0731-5090 LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byRobust Near-Optimal Aerocapture Guidance Method Based on Saturation Function13 November 2022 | Applied Sciences, Vol. 12, No. 22Aerogravity-assist capture into the three-body system: A preliminary designActa Astronautica, Vol. 198Rapid Construction of Aerocapture Attainability Sets Using Sequential Convex Programming24 June 2022 | Applied Sciences, Vol. 12, No. 13Transfer between libration orbits through the outer branches of manifolds for Phobos explorationActa Astronautica, Vol. 2Mars High Orbit Capture Using Manifolds in the Sun–Mars SystemXiangyu Li, Dong Qiao and Christian Circi2 April 2020 | Journal of Guidance, Control, and Dynamics, Vol. 43, No. 7 What's Popular Volume 42, Number 5May 2019 CrossmarkInformationCopyright © 2019 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. TopicsAerospace SciencesAstrodynamicsAstronauticsOrbital ManeuversOrbital PropertyPlanetary Science and ExplorationPlanetsSpace MissionsSpace OrbitSpace Science and Technology KeywordsOrbital EccentricitySphere of InfluenceEarthInterplanetary TrajectoriesPropellantElliptical OrbitLagrange PointsMars MissionsSolar SystemAcknowledgmentsThis work was supported by the National Natural Science Foundation of China (grants 11572038 and 11772050), Chang Jiang Scholars Program, the Discipline Innovative Engineering Plan (111 Project), and the Graduate Technological Innovation Project of Beijing Institute of Technology.PDF Received1 August 2018Accepted24 December 2018Published online19 February 2019