dc.contributorUniversidade Estadual Paulista (UNESP)
dc.creatorSantos, Josué Cardoso dos
dc.creatorZanardi, Maria Cecilia
dc.creatorMatos, Nicholas
dc.date2014-12-03T13:08:44Z
dc.date2016-10-25T20:08:47Z
dc.date2014-12-03T13:08:44Z
dc.date2016-10-25T20:08:47Z
dc.date2013-01-01
dc.date.accessioned2017-04-06T06:13:53Z
dc.date.available2017-04-06T06:13:53Z
dc.identifierXvi Brazilian Colloquium On Orbital Dynamics. Bristol: Iop Publishing Ltd, v. 465, 6 p., 2013.
dc.identifier1742-6588
dc.identifierhttp://hdl.handle.net/11449/111528
dc.identifierhttp://acervodigital.unesp.br/handle/11449/111528
dc.identifier10.1088/1742-6596/465/1/012012
dc.identifierWOS:000326877000012
dc.identifierWOS000326877000012.pdf
dc.identifierhttp://dx.doi.org/10.1088/1742-6596/465/1/012012
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/922304
dc.descriptionThis study at aims performing the stability analysis of the rotational motion to artificial satellites using quaternions to describe the satellite attitude (orientation on the space). In the system of rotational motion equations, which is composed by four kinematic equations of the quaternions and by the three Euler equations in terms of the rotational spin components. The influence of the gravity gradient and the direct solar radiation pressure torques have been considered. Equilibrium points were obtained through numerical simulations using the softwares Matlab and Octave, which are then analyzed by the Routh-Hurwitz Stability Criterion.
dc.languageeng
dc.publisherIop Publishing Ltd
dc.relationXvi Brazilian Colloquium On Orbital Dynamics
dc.rightsinfo:eu-repo/semantics/openAccess
dc.titleSemi-analytical study of the rotational motion stability of artificial satellites using quaternions
dc.typeOtro


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