Show simple item record

dc.contributor.authorBueno, Douglas D. [UNESP]
dc.contributor.authorGonsalez Bueno, Camila G. [UNESP]
dc.contributor.authorDowell, Earl H.
dc.date.accessioned2021-06-25T10:19:19Z
dc.date.available2021-06-25T10:19:19Z
dc.date.issued2021-01-01
dc.identifierhttp://dx.doi.org/10.1007/s40430-020-02754-z
dc.identifier.citationJournal of the Brazilian Society of Mechanical Sciences and Engineering, v. 43, n. 1, 2021.
dc.identifier.issn1806-3691
dc.identifier.issn1678-5878
dc.identifier.urihttp://hdl.handle.net/11449/205668
dc.description.abstractFlutter is an important topic to be considered during an aircraft development mainly due to its potentially catastrophic behavior. Typically a new aerial vehicle can require the addition of mass and limitations on its flight envelope to be flutter free. As an alternative, active control technologies can be used employing actuators and sources of power, and there are different techniques for computing the actuator’s force. In general, many approaches depend on describing the aeroelastic system through the state-space representation in the time domain. However, the state-space dynamic matrix typically contains nonphysical eigenvalues due to the unsteady aerodynamic forces approximations. In this context, this article introduces an algebraic arrangement for designing a modal controller to suppress the flutter phenomenon. The approach considers the modal state-space realization combined with the linear quadratic regulator to compute a control gain. The gain is converted from the new modal domain to the physical, and the control force introduces an effect of incremental damping for all flight envelope, although the controller is designed particularly for the flutter speed. To demonstrate the approach, numerical simulations are carried out considering the three-degree-of-freedom airfoil. The results show that this technique allows stabilizing the system.en
dc.description.sponsorshipFundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)
dc.language.isoeng
dc.relation.ispartofJournal of the Brazilian Society of Mechanical Sciences and Engineering
dc.sourceScopus
dc.subjectAeroelastic modal model
dc.subjectControl design
dc.subjectFlutter suppression
dc.subjectTransformation similarity
dc.titleA modal approach for designing controllers for active flutter suppressionen
dc.typeArtigo
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)
dc.contributor.institutionDuke University
dc.description.affiliationSchool of Engineering of Ilha Solteira São Paulo State University (UNESP), Ilha Solteira
dc.description.affiliationPratt School of Engineering Duke University
dc.description.affiliationUnespSchool of Engineering of Ilha Solteira São Paulo State University (UNESP), Ilha Solteira
dc.identifier.doi10.1007/s40430-020-02754-z
dc.description.sponsorshipIdFAPESP: 18/25194-6
dc.identifier.scopus2-s2.0-85098624958
unesp.author.orcid0000-0002-1783-0524[1]
Localize o texto completo

Files in this item

FilesSizeFormatView

There are no files associated with this item.

This item appears in the following Collection(s)

Show simple item record