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dc.contributor.authorJorba, Angel
dc.contributor.authorVillanueva Castelltort, Jordi
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Matemàtica Aplicada I
dc.date.accessioned2007-05-02T17:01:15Z
dc.date.available2007-05-02T17:01:15Z
dc.date.issued1995
dc.identifier.urihttp://hdl.handle.net/2117/848
dc.description.abstractIn this work we study the dynamics around an elliptic periodic orbit of Hamiltonian systems. To this end we have developped an algorithm to compute a normal form (up to a finite order) around this orbit, that gives an accurate description of the dynamics close to it. If the remainder of this normal form can be bounded, it is not difficult to produce explicit bounds of the diffusion time of trajectories starting near the periodic orbit. In order to discuss the effectivity of the method, it will be explained at the same time that it is applied to a concrete example. The one used here has been the Spatial Restricted Three Body Problem (RTBP)
dc.format.extent5 p.
dc.language.isoeng
dc.rightsAttribution-NonCommercial-NoDerivs 2.5 Spain
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/2.5/es/
dc.subject.lcshDynamics
dc.subject.otherperiodic orbits
dc.subject.othernormal forms
dc.subject.othereffective stability
dc.subject.otherinvariant tori
dc.titleEffective Stability Around Periodic Orbits of the Spatial RTBP
dc.typeArticle
dc.subject.lemacPartícules (Física nuclear)
dc.contributor.groupUniversitat Politècnica de Catalunya. EGSA - Equacions Diferencials, Geometria, Sistemes Dinàmics i de Control, i Aplicacions
dc.subject.amsClassificació AMS::70 Mechanics of particles and systems::70F Dynamics of a system of particles, including celestial mechanics
dc.rights.accessOpen Access
local.personalitzacitaciotrue


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