Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.14365/6455
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dc.contributor.authorPinto, Fabrizio-
dc.date.accessioned2025-09-25T19:03:51Z-
dc.date.available2025-09-25T19:03:51Z-
dc.date.issued2025-
dc.identifier.isbn9798331501525-
dc.identifier.urihttps://doi.org/10.1109/MetroAeroSpace64938.2025.11114659-
dc.identifier.urihttps://hdl.handle.net/20.500.14365/6455-
dc.description.abstractWe present advances in the accurate multiphysics modeling of nano-accelerometers motivated by the specific navigational requirements of small spacecraft under low thrust in interplanetary missions. The process of energy transfer to the nanodevice via parametric coupling is analyzed from the thermodynamical standpoint. The system is based on simultaneous electrostatic excitation and on van der Waals forces modulated by laser radiation acting as a parametric pump. It is shown that the processes involved rigorously satisfy the First and Second Laws of Thermodynamics. This proof paves the way for the design of thermodynamically consistent models of this novel class of nano-accelerometers. © 2025 Elsevier B.V., All rights reserved.en_US
dc.language.isoenen_US
dc.publisherInstitute of Electrical and Electronics Engineers Inc.en_US
dc.relation.ispartof12th IEEE International Workshop on Metrology for Aerospace (MetroAeroSpace 2025) — Naples, Italyen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectDispersion Force Engineeringen_US
dc.subjectHigh-Precision Inertial Sensorsen_US
dc.subjectLow-Thrust Propulsionen_US
dc.subjectUltra-Sensitive Geodesyen_US
dc.subjectDispersionsen_US
dc.subjectElectric Excitationen_US
dc.subjectEnergy Transferen_US
dc.subjectGeodesyen_US
dc.subjectInertial Navigation Systemsen_US
dc.subjectInterplanetary Flighten_US
dc.subjectInterplanetary Spacecraften_US
dc.subjectNanosensorsen_US
dc.subjectPrecision Engineeringen_US
dc.subjectRoboticsen_US
dc.subjectSolid-State Sensorsen_US
dc.subjectSpacecraft Propulsionen_US
dc.subjectThermodynamicsen_US
dc.subjectDispersion Forceen_US
dc.subjectDispersion Force Engineeringen_US
dc.subjectHigh-Accuracyen_US
dc.subjectHigh-Precisionen_US
dc.subjectHigh-Precision Inertial Sensoren_US
dc.subjectInertial Sensoren_US
dc.subjectLow-Thrust Propulsionen_US
dc.subjectNano-Sensorsen_US
dc.subjectUltra-Sensitive Geodesyen_US
dc.subjectUltrasensitiveen_US
dc.subjectVan Der Waals Forcesen_US
dc.titleAdvances in the Formulation of Minimal Thermodynamically Consistent Models for Dispersion Force-Driven High-Accuracy Inertial Nano-Sensorsen_US
dc.typeConference Objecten_US
dc.identifier.doi10.1109/MetroAeroSpace64938.2025.11114659-
dc.identifier.scopus2-s2.0-105015443428-
dc.departmentİzmir Ekonomi Üniversitesien_US
dc.authorscopusid8638997200-
dc.identifier.startpage87en_US
dc.identifier.endpage92en_US
dc.institutionauthorPinto, Fabrizio-
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
dc.identifier.scopusqualityN/A-
dc.identifier.wosqualityN/A-
item.languageiso639-1en-
item.fulltextNo Fulltext-
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
item.grantfulltextnone-
item.openairetypeConference Object-
item.cerifentitytypePublications-
crisitem.author.dept05.01. Aerospace Engineering-
Appears in Collections:Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection
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