DC Field | Value | Language |
---|---|---|
dc.contributor.author | Lee, Jinsung | ko |
dc.contributor.author | Sung, Taehyun | ko |
dc.contributor.author | Ahn, Jaemyung | ko |
dc.date.accessioned | 2024-06-10T15:00:37Z | - |
dc.date.available | 2024-06-10T15:00:37Z | - |
dc.date.created | 2023-08-23 | - |
dc.date.issued | 2024-01 | - |
dc.identifier.citation | INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.25, no.1, pp.229 - 249 | - |
dc.identifier.issn | 2093-274X | - |
dc.identifier.uri | http://hdl.handle.net/10203/319727 | - |
dc.description.abstract | This 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.language | English | - |
dc.publisher | SPRINGER | - |
dc.title | Manifold-Based Space Mission Design with Poincaré Filtering Algorithm | - |
dc.type | Article | - |
dc.identifier.wosid | 001049927800001 | - |
dc.type.rims | ART | - |
dc.citation.volume | 25 | - |
dc.citation.issue | 1 | - |
dc.citation.beginningpage | 229 | - |
dc.citation.endingpage | 249 | - |
dc.citation.publicationname | INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES | - |
dc.identifier.doi | 10.1007/s42405-023-00651-y | - |
dc.contributor.localauthor | Ahn, Jaemyung | - |
dc.description.isOpenAccess | N | - |
dc.type.journalArticle | Article; Early Access | - |
dc.subject.keywordAuthor | Poincare filter | - |
dc.subject.keywordAuthor | Manifold | - |
dc.subject.keywordAuthor | Lagrange point | - |
dc.subject.keywordAuthor | Trajectory design | - |
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