Modified equations of motion around circular trajectory and its application to formation flying control

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dc.contributor.authorKawaguchi, Jun'ichiroen
dc.date.accessioned2026-01-01T13:41:01Z
dc.date.available2026-01-01T13:41:01Z
dc.date.issued2007en
dc.description.abstractUsually, the formation flying associated with a circular orbit is discussed through the well-known Hill's equations of motion. This paper presents and discusses the formation-fixed coordinate to discuss about the formation behavior. The resulted equations take the non-autonomous form and will depict some interesting characteristics. The paper will also present the application of decentralized formation control strategy that stabilizes and enables a quick reaction to the command.en
dc.description.statusPeer-revieweden
dc.format.extent6en
dc.identifier.isbn9780877035411en
dc.identifier.issn0065-3438en
dc.identifier.otherORCID:/0000-0001-8196-5194/work/162948020en
dc.identifier.scopus55849083969en
dc.identifier.urihttps://hdl.handle.net/1885/733800570
dc.language.isoenen
dc.relation.ispartofAmerican Astronautical Society - Space Flight Mechanics 2007 - Advances in the Astronautical Sciences, Proceedings of the AAS/AIAA Space Flight Mechanics Meetingen
dc.relation.ispartofseries17th Annual Space Flight Mechanics Meetingen
dc.relation.ispartofseriesAdvances in the Astronautical Sciencesen
dc.titleModified equations of motion around circular trajectory and its application to formation flying controlen
dc.typeConference paperen
dspace.entity.typePublicationen
local.bibliographicCitation.lastpage1434en
local.bibliographicCitation.startpage1429en
local.contributor.affiliationKawaguchi, Jun'ichiro; JAXA Institute of Space and Astronautical Scienceen
local.identifier.pure3b635f7f-203a-40f4-8162-9fd873b5b2b9en
local.identifier.urlhttps://www.scopus.com/pages/publications/55849083969en
local.type.statusPublisheden

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