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dc.contributorEscuela Superior y Tecnica de Ingenieros de Minases_ES
dc.contributor.authorGarcía Nieto, Paulino José
dc.contributor.authorGarcía Gonzalo, Esperanza
dc.contributor.authorBernardo Sánchez, Antonio 
dc.contributor.authorMenéndez Fernández, Marta 
dc.contributor.otherExplotacion de Minases_ES
dc.date2016-05-26
dc.date.accessioned2023-12-22T09:56:05Z
dc.date.available2023-12-22T09:56:05Z
dc.identifier.citationGarcia Nieto, P. J., García-Gonzalo, E., Bernardo Sanchez, A., & Menendez Fernandez, M. (2016). A new predictive model based on the ABC optimized multivariate adaptive regression splines approach for predicting the remaining useful life in aircraft engines. Energies, 9(6), 409.es_ES
dc.identifier.urihttps://hdl.handle.net/10612/17524
dc.description.abstract[EN] Remaining useful life (RUL) estimation is considered as one of the most central points in the prognostics and health management (PHM). The present paper describes a nonlinear hybrid ABC–MARS-based model for the prediction of the remaining useful life of aircraft engines. Indeed, it is well-known that an accurate RUL estimation allows failure prevention in a more controllable way so that the effective maintenance can be carried out in appropriate time to correct impending faults. The proposed hybrid model combines multivariate adaptive regression splines (MARS), which have been successfully adopted for regression problems, with the artificial bee colony (ABC) technique. This optimization technique involves parameter setting in the MARS training procedure, which significantly influences the regression accuracy. However, its use in reliability applications has not yet been widely explored. Bearing this in mind, remaining useful life values have been predicted here by using the hybrid ABC–MARS-based model from the remaining measured parameters (input variables) for aircraft engines with success. A correlation coefficient equal to 0.92 was obtained when this hybrid ABC–MARS-based model was applied to experimental data. The agreement of this model with experimental data confirmed its good performance. The main advantage of this predictive model is that it does not require information about the previous operation states of the aircraft engine.es_ES
dc.languageenges_ES
dc.publisherMDPIes_ES
dc.subjectAeronáuticaes_ES
dc.subjectMecánicaes_ES
dc.subject.otherMultivariate adaptive regression splines (MARS)es_ES
dc.subject.otherArtificial bee colony (ABC)es_ES
dc.subject.otherAircraft enginees_ES
dc.subject.otherRemaining useful life (RUL)es_ES
dc.subject.otherPrognosticses_ES
dc.subject.otherReliabilityes_ES
dc.titleA New Predictive Model Based on the ABC Optimized Multivariate Adaptive Regression Splines Approach for Predicting the Remaining Useful Life in Aircraft Engineses_ES
dc.typeinfo:eu-repo/semantics/articlees_ES
dc.identifier.doi10.3390/en9060409
dc.description.peerreviewedSIes_ES
dc.rights.accessRightsinfo:eu-repo/semantics/openAccesses_ES
dc.identifier.essn1996-1073
dc.journal.titleEnergieses_ES
dc.volume.number9es_ES
dc.issue.number6es_ES
dc.page.initial19es_ES
dc.type.hasVersioninfo:eu-repo/semantics/publishedVersiones_ES
dc.subject.unesco3301.15 Sistemas de Propulsiónes_ES


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