dc.creator | Vázquez Valenzuela, Rafael | es |
dc.creator | Gavilán Jiménez, Francisco | es |
dc.creator | Camacho, Eduardo F. | es |
dc.date.accessioned | 2020-03-06T07:57:13Z | |
dc.date.available | 2020-03-06T07:57:13Z | |
dc.date.issued | 2017 | |
dc.identifier.citation | Vázquez Valenzuela, R., Gavilán Jiménez, F. y Fernández Camacho, E. (2017). Pulse-width predictive control for LTV systems with application to spacecraft rendezvous. Control Engineering Practice, 60, 199-210. | |
dc.identifier.issn | 0967-0661 | es |
dc.identifier.uri | https://hdl.handle.net/11441/93969 | |
dc.description.abstract | This work presents a Model Predictive Controller (MPC) that is able to handle Linear Time-Varying (LTV) plants with Pulse-Width Modulated (PWM) control. The MPC is based on a planner that employs a Pulse-Amplitude Modulated (PAM) or impulsive approximation as a hot-start and then uses explicit linearization around successive PWM solutions for rapidly improving the solution by means of quadratic programming. As an example, the problem of rendezvous of spacecraft for eccentric target orbits is considered. The problem is modeled by the LTV Tschauner–Hempel equations, whose state transition matrix is explicit; this is exploited by the algorithm for rapid convergence. The efficacy of the method is shown in a simulation study. | es |
dc.description.sponsorship | Ministerio de Economía y Competitividad DPI2008–05818 | es |
dc.description.sponsorship | Ministerio de Economía y Competitividad MTM2015-65608-P | es |
dc.format | application/pdf | es |
dc.format.extent | 11 p. | es |
dc.language.iso | eng | es |
dc.publisher | Elsevier | es |
dc.relation.ispartof | Control Engineering Practice, 60, 199-210. | |
dc.rights | Attribution-NonCommercial-NoDerivatives 4.0 Internacional | * |
dc.rights.uri | http://creativecommons.org/licenses/by-nc-nd/4.0/ | * |
dc.subject | Spacecraft autonomy | es |
dc.subject | Space robotics | es |
dc.subject | Pulse-width modulation | es |
dc.title | Pulse-width predictive control for LTV systems with application to spacecraft rendezvous | es |
dc.type | info:eu-repo/semantics/article | es |
dcterms.identifier | https://ror.org/03yxnpp24 | |
dc.type.version | info:eu-repo/semantics/submittedVersion | es |
dc.rights.accessRights | info:eu-repo/semantics/openAccess | es |
dc.contributor.affiliation | Universidad de Sevilla. Departamento de Ingeniería de Sistemas y Automática | es |
dc.contributor.affiliation | Universidad de Sevilla. Departamento de Ingeniería Aeroespacial y Mecánica de Fluidos | es |
dc.relation.publisherversion | https://www.sciencedirect.com/science/article/pii/S0967066116301381#! | es |
dc.identifier.doi | https://www.sciencedirect.com/science/article/pii/S0967066116301381#! | es |
dc.journaltitle | Control Engineering Practice | es |
dc.publication.volumen | 60 | es |
dc.publication.initialPage | 199 | es |
dc.publication.endPage | 210 | es |
dc.identifier.sisius | 20978105 | es |
dc.contributor.funder | DPI2008–05818 | es |
dc.contributor.funder | MTM2015-65608-P | es |