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dc.contributor.authorStefania, Soldini
dc.contributor.authorGomez Muntané, Gerard
dc.contributor.authorMasdemont Soler, Josep
dc.contributor.authorCamilla, Colombo
dc.contributor.authorWalker, Scott
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Matemàtiques
dc.date.accessioned2017-03-13T11:30:03Z
dc.date.issued2016
dc.identifier.citationStefania, S., Gomez Muntané, Gerard, Masdemont, J.J., Camilla, C., Walker, S. Solar radiation pressure assisted transfers between Lissajous orbits of the Sun-Earth system. A: International Astronautical Congress. "67th International Astronautical Congress (IAC), Guadalajara, Mexico, 26-30 September 2016". Guadalajara: 2016, p. 1-18.
dc.identifier.urihttp://hdl.handle.net/2117/102382
dc.description.abstractThis article investigates a propellant-free transfer between Lissa jous orbits in the Sun-Earth system modelled as a photo-gravitational circular restricted three body p roblem. The geometry of the phase space around the L 1 , 2 equilibrium points is exploited to change the amplitudes and phases of the initial Lissajous orbit using the associated hyperbolic invarian t manifolds. The desired Lissajous orbit is reached by cancelling out the instabilities by means o f solar radiation pressure manoeuvres. The acceleration required is controlled by the change in the spacecraft’s reflectivity and angle of incidence of the Sun-line direction. Changes in reflectivit y allow transfers along the x -axis, while re-orientations of the spacecraft move the equilibrium p oints, and the orbits around them, towards the x - y plane. For equilibrium points in the x - y plane, the in-plane centre manifold tends to a center × centre × focus equilibrium. The analytical solution is extended to this general case. An analysis in the magnitude of the manoeuvre required is pres ented for different Lissajous orbit amplitudes and reflectivity, along with a comment on harnessing solar radiation pressure devices
dc.format.extent18 p.
dc.language.isoeng
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/es/
dc.subjectÀrees temàtiques de la UPC::Matemàtiques i estadística
dc.subject.lcshThree-body problem
dc.subject.lcshOrbits
dc.subject.lcshAtmospheric physics
dc.titleSolar radiation pressure assisted transfers between Lissajous orbits of the Sun-Earth system
dc.typeConference report
dc.subject.lemacProblema dels tres cossos
dc.subject.lemacÒrbites -- Congressos
dc.contributor.groupUniversitat Politècnica de Catalunya. SD - Sistemes Dinàmics de la UPC
dc.rights.accessRestricted access - publisher's policy
drac.iddocument19707164
dc.description.versionPostprint (author's final draft)
dc.date.lift10000-01-01
upcommons.citation.authorStefania, S., Gomez Muntané, Gerard, Masdemont, J.J., Camilla, C., Walker, S.
upcommons.citation.contributorInternational Astronautical Congress
upcommons.citation.pubplaceGuadalajara
upcommons.citation.publishedtrue
upcommons.citation.publicationName67th International Astronautical Congress (IAC), Guadalajara, Mexico, 26-30 September 2016
upcommons.citation.startingPage1
upcommons.citation.endingPage18


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