dc.creator | Sánchez Merino, Julio César | es |
dc.creator | Louembet, Christophe | es |
dc.creator | Gavilán Jiménez, Francisco | es |
dc.creator | Vázquez Valenzuela, Rafael | es |
dc.date.accessioned | 2022-01-12T16:38:13Z | |
dc.date.available | 2022-01-12T16:38:13Z | |
dc.date.issued | 2021 | |
dc.identifier.citation | Sánchez 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.issn | 0731-5090 | es |
dc.identifier.uri | https://hdl.handle.net/11441/128798 | |
dc.description.abstract | This 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 discussed | es |
dc.description.sponsorship | Ministerio de Ciencia e Innovación (España) PGC2018-100680-B-C21 | es |
dc.description.sponsorship | Universidad de Sevilla PP2016-6975 | es |
dc.format | application/pdf | es |
dc.format.extent | 17 p. | es |
dc.language.iso | eng | es |
dc.publisher | AIAA International | es |
dc.relation.ispartof | Journal of Guidance, Control, and Dynamics, 44 (10), 1794-1810. | |
dc.rights | Attribution-NonCommercial-NoDerivatives 4.0 Internacional | * |
dc.rights.uri | http://creativecommons.org/licenses/by-nc-nd/4.0/ | * |
dc.subject | Computation theory | es |
dc.subject | Computational efficiency | es |
dc.subject | Control theory | es |
dc.subject | Impulse response | es |
dc.subject | Space rendezvous | es |
dc.title | Event-based impulsive control for spacecraft rendezvous hovering phases | es |
dc.type | info:eu-repo/semantics/article | es |
dcterms.identifier | https://ror.org/03yxnpp24 | |
dc.type.version | info:eu-repo/semantics/publishedVersion | es |
dc.rights.accessRights | info:eu-repo/semantics/openAccess | es |
dc.contributor.affiliation | Universidad de Sevilla. Departamento de Ingeniería Aeroespacial y Mecánica de Fluidos | es |
dc.relation.projectID | PGC2018-100680-B-C21 | es |
dc.relation.projectID | PP2016-6975 | es |
dc.relation.publisherversion | https://arc.aiaa.org/doi/10.2514/1.G005507 | es |
dc.identifier.doi | 10.2514/1.G005507 | es |
dc.journaltitle | Journal of Guidance, Control, and Dynamics | es |
dc.publication.volumen | 44 | es |
dc.publication.issue | 10 | es |
dc.publication.initialPage | 1794 | es |
dc.publication.endPage | 1810 | es |