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Dynamics of a gyrostat satellite with the vector of gyrostatic moment tangent to the orbital plane

dc.contributor.authorMorais, Renato
dc.contributor.authorSantos, Luis
dc.contributor.authorSilva, André
dc.contributor.authorMelício, Rui
dc.date.accessioned2022-03-29T08:38:15Z
dc.date.available2024-03-12T01:30:22Z
dc.date.issued2022-03-12
dc.description.abstractIn this paper, a gyrostat satellite in a circular orbit with its gyrostatic moment tangent to the orbital plane and collinear with the orbital speed is studied regarding its equilibria, bifurcation of equilibria, and asymptotic stability conditions. In the general case, where any gyrostat angular momentum is aligned with any of the orbital coordinate frames, interesting results arose regarding its equilibria bifurcation regarding conditions near to the ones presented in this paper, namely equilibria regions outside their main regions near to the orbital plane tangent. For equilibria and bifurcation of equilibria, a symbolic-numerical method is used to obtain the polynomial equations in function of non-dimensional parameters whose roots are equivalent to the number of equilibria positions. For the asymptotic stability, the results are tested using the Lyapunov stability theory scheme.pt_PT
dc.description.sponsorshipFundação para a Ciência e a Tecnologiapt_PT
dc.description.versioninfo:eu-repo/semantics/publishedVersionpt_PT
dc.identifier.citationR. H. Morais, L. F. F. M. Santos, A. R. R. Silva et al., Dynamics of a gyrostat satellite with the vector of gyrostatic moment tangent to the orbital plane, Advances in Space Research, https://doi.org/10.1016/j.asr.2022.03.004pt_PT
dc.identifier.doi10.1016/j.asr.2022.03.004pt_PT
dc.identifier.issn0273-1177
dc.identifier.urihttp://hdl.handle.net/10400.6/12122
dc.language.isoengpt_PT
dc.peerreviewedyespt_PT
dc.publisherElsevier B. V.pt_PT
dc.relationAssociate Laboratory of Energy, Transports and Aeronautics
dc.relationINSTITUTE OF EARTH SCIENCES
dc.relation.publisherversionhttps://doi.org/10.1016/j.asr.2022.03.004pt_PT
dc.subjectAerospace Dynamicspt_PT
dc.subjectEquilibriumpt_PT
dc.subjectEquilibriumpt_PT
dc.subjectStabilisationpt_PT
dc.subjectBifurcation of Equilibriapt_PT
dc.titleDynamics of a gyrostat satellite with the vector of gyrostatic moment tangent to the orbital planept_PT
dc.typejournal article
dspace.entity.typePublication
oaire.awardTitleAssociate Laboratory of Energy, Transports and Aeronautics
oaire.awardTitleINSTITUTE OF EARTH SCIENCES
oaire.awardURIinfo:eu-repo/grantAgreement/FCT/6817 - DCRRNI ID/UIDB%2F50022%2F2020/PT
oaire.awardURIinfo:eu-repo/grantAgreement/FCT/6817 - DCRRNI ID/UIDB%2F04683%2F2020/PT
oaire.citation.titleAdvances in Space Researchpt_PT
oaire.fundingStream6817 - DCRRNI ID
oaire.fundingStream6817 - DCRRNI ID
person.familyNameMorais
person.familyNameSantos
person.familyNameResende Rodrigues da Silva
person.familyNameMelício
person.givenNameRenato
person.givenNameLuis
person.givenNameAndré
person.givenNameRui
person.identifierJ-4185-2012
person.identifier.ciencia-idD516-971F-D3B0
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person.identifier.ciencia-id8219-4B2B-E1C7
person.identifier.ciencia-idA213-8E2D-0102
person.identifier.orcid0000-0002-6980-4280
person.identifier.orcid0000-0002-7169-2660
person.identifier.orcid0000-0002-4901-7140
person.identifier.orcid0000-0002-1081-2729
person.identifier.ridI-6614-2015
person.identifier.scopus-author-id12768907700
person.identifier.scopus-author-id11440407500
project.funder.identifierhttp://doi.org/10.13039/501100001871
project.funder.identifierhttp://doi.org/10.13039/501100001871
project.funder.nameFundação para a Ciência e a Tecnologia
project.funder.nameFundação para a Ciência e a Tecnologia
rcaap.embargofctpublicação sem custos para os autores.pt_PT
rcaap.rightsopenAccesspt_PT
rcaap.typearticlept_PT
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