On the station keeping of a Solar sail in the Elliptic Sun-Earth system

In this work we focus on the dynamics of a solar sail in the Sun Earth Elliptic Restricted Three-Body Problem with solar radiation pressure. The considered situation is the motion of a sail close to the $L_{1}$ point, but displacing the equilibrium point with the sail so that it is possible to have...

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Detalles Bibliográficos
Autores: Farrés Basiana, Ariadna, Jorba i Monte, Àngel
Tipo de recurso: artículo
Estado:Versión aceptada para publicación
Fecha de publicación:2011
País:España
Institución:Universidad de Barcelona
Repositorio:Dipòsit Digital de la UB
OAI Identifier:oai:diposit.ub.edu:2445/165982
Acceso en línea:https://hdl.handle.net/2445/165982
Access Level:acceso abierto
Palabra clave:Mecànica celeste
Òrbites
Dinàmica
Celestial mechanics
Orbits
Dynamics
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spelling On the station keeping of a Solar sail in the Elliptic Sun-Earth systemFarrés Basiana, AriadnaJorba i Monte, ÀngelMecànica celesteÒrbitesDinàmicaCelestial mechanicsOrbitsDynamicsIn this work we focus on the dynamics of a solar sail in the Sun Earth Elliptic Restricted Three-Body Problem with solar radiation pressure. The considered situation is the motion of a sail close to the $L_{1}$ point, but displacing the equilibrium point with the sail so that it is possible to have continuous communication with the Earth. In previous works we derived a station keeping strategy for this situation but using the Circular RTBP as a model. In this paper we discuss the effect of the eccentricity in the region close to the sail-displaced $L_{1}$ point of the Circular RTBP. Then we show how to use the information on this dynamics to design a station keeping strategy. Finally, we apply these results to the GeoStorm mission, including errors in the sail orientation and on the estimation of the position of the sail in the simulations.Elsevier2011info:eu-repo/semantics/articleinfo:eu-repo/semantics/acceptedVersionapplication/pdfhttps://hdl.handle.net/2445/165982Articles publicats en revistes (Matemàtiques i Informàtica)reponame:Dipòsit Digital de la UBinstname:Universidad de BarcelonaInglésVersió postprint del document publicat a: https://doi.org/10.1016/j.asr.2011.02.004Advances in Space Research, 2011, vol. 48, num. 11, p. 1785-1796https://doi.org/10.1016/j.asr.2011.02.004(c) COSPAR, 2011info:eu-repo/semantics/openAccessoai:diposit.ub.edu:2445/1659822026-05-27T06:46:51Z
dc.title.none.fl_str_mv On the station keeping of a Solar sail in the Elliptic Sun-Earth system
title On the station keeping of a Solar sail in the Elliptic Sun-Earth system
spellingShingle On the station keeping of a Solar sail in the Elliptic Sun-Earth system
Farrés Basiana, Ariadna
Mecànica celeste
Òrbites
Dinàmica
Celestial mechanics
Orbits
Dynamics
title_short On the station keeping of a Solar sail in the Elliptic Sun-Earth system
title_full On the station keeping of a Solar sail in the Elliptic Sun-Earth system
title_fullStr On the station keeping of a Solar sail in the Elliptic Sun-Earth system
title_full_unstemmed On the station keeping of a Solar sail in the Elliptic Sun-Earth system
title_sort On the station keeping of a Solar sail in the Elliptic Sun-Earth system
dc.creator.none.fl_str_mv Farrés Basiana, Ariadna
Jorba i Monte, Àngel
author Farrés Basiana, Ariadna
author_facet Farrés Basiana, Ariadna
Jorba i Monte, Àngel
author_role author
author2 Jorba i Monte, Àngel
author2_role author
dc.subject.none.fl_str_mv Mecànica celeste
Òrbites
Dinàmica
Celestial mechanics
Orbits
Dynamics
topic Mecànica celeste
Òrbites
Dinàmica
Celestial mechanics
Orbits
Dynamics
description In this work we focus on the dynamics of a solar sail in the Sun Earth Elliptic Restricted Three-Body Problem with solar radiation pressure. The considered situation is the motion of a sail close to the $L_{1}$ point, but displacing the equilibrium point with the sail so that it is possible to have continuous communication with the Earth. In previous works we derived a station keeping strategy for this situation but using the Circular RTBP as a model. In this paper we discuss the effect of the eccentricity in the region close to the sail-displaced $L_{1}$ point of the Circular RTBP. Then we show how to use the information on this dynamics to design a station keeping strategy. Finally, we apply these results to the GeoStorm mission, including errors in the sail orientation and on the estimation of the position of the sail in the simulations.
publishDate 2011
dc.date.none.fl_str_mv 2011
dc.type.none.fl_str_mv info:eu-repo/semantics/article
info:eu-repo/semantics/acceptedVersion
format article
status_str acceptedVersion
dc.identifier.none.fl_str_mv https://hdl.handle.net/2445/165982
url https://hdl.handle.net/2445/165982
dc.language.none.fl_str_mv Inglés
language_invalid_str_mv Inglés
dc.relation.none.fl_str_mv Versió postprint del document publicat a: https://doi.org/10.1016/j.asr.2011.02.004
Advances in Space Research, 2011, vol. 48, num. 11, p. 1785-1796
https://doi.org/10.1016/j.asr.2011.02.004
dc.rights.none.fl_str_mv (c) COSPAR, 2011
info:eu-repo/semantics/openAccess
rights_invalid_str_mv (c) COSPAR, 2011
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv Elsevier
publisher.none.fl_str_mv Elsevier
dc.source.none.fl_str_mv Articles publicats en revistes (Matemàtiques i Informàtica)
reponame:Dipòsit Digital de la UB
instname:Universidad de Barcelona
instname_str Universidad de Barcelona
reponame_str Dipòsit Digital de la UB
collection Dipòsit Digital de la UB
repository.name.fl_str_mv
repository.mail.fl_str_mv
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score 15,300719

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