Manifold-Based Space Mission Design with Poincaré Filtering Algorithm

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dc.contributor.authorLee, Jinsungko
dc.contributor.authorSung, Taehyunko
dc.contributor.authorAhn, Jaemyungko
dc.date.accessioned2024-06-10T15:00:37Z-
dc.date.available2024-06-10T15:00:37Z-
dc.date.created2023-08-23-
dc.date.issued2024-01-
dc.identifier.citationINTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.25, no.1, pp.229 - 249-
dc.identifier.issn2093-274X-
dc.identifier.urihttp://hdl.handle.net/10203/319727-
dc.description.abstractThis paper presents the application of manifolds for space mission design in the Circular Restricted Three Body Problem, Bi-Circular Restricted Four Body Problem, and Patched-Planar Circular Restricted Three Body Problem. We tackle these three types of missions by defining each mission's manifold-based transfer roadmap/sequence. The transfer to Sun-Earth L4 and L5 planar Lyapunov orbits utilizing the electric-propulsion-system-assisted artificial stable manifolds and the Sun-Earth system's L1 and L2 stable and unstable manifolds are designed utilizing the circular restricted three-body problem. We also design the weak stability boundary transfers to Earth-Moon's L1 and L2 utilizing Earth-Moon's stable manifold and Sun-Earth's L1 and L2 unstable manifolds utilizing the Bi-Circular Restricted Four Body Problem. We present a manifold projection method to quickly assess manifold reachability for multiple-moon tour analysis utilizing the patched-planar circular restricted three-body problem. A new filter is used during the Poincare section analysis to determine optimal sets of stable and unstable manifolds for several types of missions. The multiple-point differential corrector is utilized with optimal manifolds to determine a continuous smooth trajectory for spacecraft with impulsive burn maneuvers.-
dc.languageEnglish-
dc.publisherSPRINGER-
dc.titleManifold-Based Space Mission Design with Poincaré Filtering Algorithm-
dc.typeArticle-
dc.identifier.wosid001049927800001-
dc.type.rimsART-
dc.citation.volume25-
dc.citation.issue1-
dc.citation.beginningpage229-
dc.citation.endingpage249-
dc.citation.publicationnameINTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES-
dc.identifier.doi10.1007/s42405-023-00651-y-
dc.contributor.localauthorAhn, Jaemyung-
dc.description.isOpenAccessN-
dc.type.journalArticleArticle; Early Access-
dc.subject.keywordAuthorPoincare filter-
dc.subject.keywordAuthorManifold-
dc.subject.keywordAuthorLagrange point-
dc.subject.keywordAuthorTrajectory design-
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AE-Journal Papers(저널논문)
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