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Transfer and stabilization in L2 small halos via low continuous thrust

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dc.contributor.authorTanaka, Keitaen
dc.contributor.authorKavvaguchi, Jun'ichiroen
dc.date.accessioned2026-01-01T13:41:11Z
dc.date.available2026-01-01T13:41:11Z
dc.date.issued2012en
dc.description.abstractThis paper discusses how to design small-halo-type periodic orbits around L1/L2 with low-level continuous thrust. It starts with formulating the problem as a trajectory optimization problem. Then we convert it into a nonlinear programing problem and solve. In addition, the ways to send spacecraft into this type of periodic orbits are also discussed. The results show the developed injection and stabilizing methods can be applicable to the actual space missions. Copyrighten
dc.description.statusPeer-revieweden
dc.format.extent5en
dc.identifier.isbn9781622769797en
dc.identifier.issn0074-1795en
dc.identifier.scopus84883531293en
dc.identifier.urihttps://hdl.handle.net/1885/733800628
dc.language.isoenen
dc.relation.ispartof63rd International Astronautical Congress 2012, IAC 2012en
dc.relation.ispartofseries63rd International Astronautical Congress 2012, IAC 2012en
dc.relation.ispartofseriesProceedings of the International Astronautical Congress, IACen
dc.titleTransfer and stabilization in L2 small halos via low continuous thrusten
dc.typeConference paperen
dspace.entity.typePublicationen
local.bibliographicCitation.lastpage5778en
local.bibliographicCitation.startpage5774en
local.contributor.affiliationTanaka, Keita; The University of Tokyoen
local.contributor.affiliationKavvaguchi, Jun'ichiro; ISAS/JAXAen
local.identifier.pureff86e48e-555f-4ecb-9672-202bd3317883en
local.identifier.urlhttps://www.scopus.com/pages/publications/84883531293en
local.type.statusPublisheden

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