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Gyrostat dynamics on a circular orbit

datacite.subject.fosCiências Naturais::Ciências Físicaspt_PT
dc.contributor.advisorSilva, André Resende Rodrigues da
dc.contributor.advisorSarychev, Vasili A.
dc.contributor.authorSantos, Luís Filipe Ferreira Marques
dc.date.accessioned2016-02-24T15:58:03Z
dc.date.available2016-02-24T15:58:03Z
dc.date.issued2015
dc.description.abstractThe attitude control of a modern satellite is a crucial condition for its operation. In this work, is investigated the dynamics of an asymmetrical inertial distribution gyrostat satellite, subjected to gravitational torque, moving along a circular orbit in a central Newtonian gravitational field. To solve the problem it is proposed a symbolic-numerical method for determining all equilibrium orientations of an asymmetrical gyrostat satellite in the orbital coordinate system with a given gyrostatic torque and given principal central moments of inertia. The conditions of equilibria are obtained depending on four dimensionless parameters of the system. The evolution of the domains in the study of equilibria and stability is carried out in great detail. All bifurcation values of parameters at which there is a change of numbers of equilibrium orientations are determined with great accuracy. For each equilibrium orientation the sufficient conditions of stability are obtained as a result of analysis of the generalized integral of energy used as a Lyapunov’s function. It is shown that the number of equilibria of a gyrostat satellite in the general case must be between 8 and 24, and that the number of stable equilibria changes from 4 to 2.pt_PT
dc.identifier.tid101410760
dc.identifier.urihttp://hdl.handle.net/10400.6/4034
dc.language.isoengpt_PT
dc.subjectVeículo espacialpt_PT
dc.subjectDinâmica girostáticapt_PT
dc.subjectAeronáutica - Satélitespt_PT
dc.titleGyrostat dynamics on a circular orbitpt_PT
dc.typedoctoral thesis
dspace.entity.typePublication
person.familyNameSantos
person.givenNameLuis
person.identifier.ciencia-id6717-B0D3-0F5B
person.identifier.orcid0000-0002-7169-2660
person.identifier.ridI-6614-2015
person.identifier.scopus-author-id12768907700
rcaap.rightsopenAccesspt_PT
rcaap.typedoctoralThesispt_PT
relation.isAuthorOfPublication58ad442e-76b5-4fe4-8cc4-0456573e5709
relation.isAuthorOfPublication.latestForDiscovery58ad442e-76b5-4fe4-8cc4-0456573e5709
thesis.degree.nameDoutoramento em Engenharia Aeronáuticapt_PT

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