Optimal time-fixed impulsive non-Keplerian orbit to orbit transfer algorithm based on primer vector theory

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dc.contributor.authorBucchioni, Giordana
dc.contributor.authorGemignani, Gabriele
dc.contributor.authorLombardi, Francesco
dc.contributor.authorBellome, Andrea
dc.contributor.authorLeitão, João Pedro Fernandes
dc.contributor.authorLizy-Destrez, Stèphanie
dc.contributor.authorInnocenti, Mario
dc.date.accessioned2023-06-07T13:35:09Z
dc.date.available2023-06-07T13:35:09Z
dc.date.issued2023-06-06
dc.description.abstractThe work applies a systematic method to compute an optimal transfer trajectory between two non-Keplerian halo orbits in the Circular Restricted Three-body formulation of the Earth–Moon dynamics. The paper exploits the knowledge of the natural non-linear dynamics and the primer vector theory applied to the Circular Restricted Three Body Problem to design optimal multi-impulsive Halo-to-Halo transfers with fixed and limited Time of flight, from every point of the departure orbit to every point of the arrival orbit with an optimal number of impulses. The used method is constituted by three systematic steps with the goal of facilitating the mission design process and the on-board autonomous guidance implementation of future missions in highly non-linear dynamics.en_UK
dc.identifier.citationBucchioni G, Geminiani G, Lombardi F, et al., (2023) Optimal time-fixed impulsive non-Keplerian orbit to orbit transfer algorithm based on primer vector theory, Communications in Nonlinear Science and Numerical Simulation, Volume 124, September 2023, Article number 107307en_UK
dc.identifier.eissn1878-7274
dc.identifier.issn1007-5704
dc.identifier.urihttps://doi.org/10.1016/j.cnsns.2023.107307
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/19760
dc.language.isoenen_UK
dc.publisherElsevieren_UK
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/*
dc.subjectCR3BPen_UK
dc.subjectHaloTransferen_UK
dc.subjectOptimisationen_UK
dc.subjectAstrodynamicsen_UK
dc.titleOptimal time-fixed impulsive non-Keplerian orbit to orbit transfer algorithm based on primer vector theoryen_UK
dc.typeArticleen_UK

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