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dc.creatorSánchez Merino, Julio Césares
dc.creatorLouembet, Christophees
dc.creatorGavilán Jiménez, Franciscoes
dc.creatorVázquez Valenzuela, Rafaeles
dc.date.accessioned2022-01-12T16:38:13Z
dc.date.available2022-01-12T16:38:13Z
dc.date.issued2021
dc.identifier.citationSánchez Merino, J.C., Louembet, C., Gavilán Jiménez, F. y Vázquez Valenzuela, R. (2021). Event-based impulsive control for spacecraft rendezvous hovering phases. Journal of Guidance, Control, and Dynamics, 44 (10), 1794-1810.
dc.identifier.issn0731-5090es
dc.identifier.urihttps://hdl.handle.net/11441/128798
dc.description.abstractThis work presents an event-triggered controller for spacecraft rendezvous hovering phases. The goal is to maintain the chaser within a bounded region with respect to the target. The main assumption is that the chaser vehicle has impulsive thrusters. These are assumed to be orientable at any direction and are constrained by dead-zone and saturation bounds. The event-based controller relies on trigger rules deciding when a suitable control law is applied. The local control law consists on a single impulse; therefore the trigger rules design is based on the instantaneous reachability to the admissible set. The final outcome is a very efficient algorithm from both computational burden and footprint perspectives. Because the proposed methodology is based on a single impulse control, the controller invariance is local and assessed through impulsive systems theory. Finally, numerical results are shown and discussedes
dc.description.sponsorshipMinisterio de Ciencia e Innovación (España) PGC2018-100680-B-C21es
dc.description.sponsorshipUniversidad de Sevilla PP2016-6975es
dc.formatapplication/pdfes
dc.format.extent17 p.es
dc.language.isoenges
dc.publisherAIAA Internationales
dc.relation.ispartofJournal of Guidance, Control, and Dynamics, 44 (10), 1794-1810.
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 Internacional*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/*
dc.subjectComputation theoryes
dc.subjectComputational efficiencyes
dc.subjectControl theoryes
dc.subjectImpulse responsees
dc.subjectSpace rendezvouses
dc.titleEvent-based impulsive control for spacecraft rendezvous hovering phaseses
dc.typeinfo:eu-repo/semantics/articlees
dcterms.identifierhttps://ror.org/03yxnpp24
dc.type.versioninfo:eu-repo/semantics/publishedVersiones
dc.rights.accessRightsinfo:eu-repo/semantics/openAccesses
dc.contributor.affiliationUniversidad de Sevilla. Departamento de Ingeniería Aeroespacial y Mecánica de Fluidoses
dc.relation.projectIDPGC2018-100680-B-C21es
dc.relation.projectIDPP2016-6975es
dc.relation.publisherversionhttps://arc.aiaa.org/doi/10.2514/1.G005507es
dc.identifier.doi10.2514/1.G005507es
dc.journaltitleJournal of Guidance, Control, and Dynamicses
dc.publication.volumen44es
dc.publication.issue10es
dc.publication.initialPage1794es
dc.publication.endPage1810es

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