2020-05-31T10:29:42Z
http://oa.upm.es/cgi/oai2
oai:oa.upm.es:21139
2016-04-21T11:14:31Z
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Dynamic stabilization of L2 periodic orbits using attitude-orbit coupling effects
Peláez Álvarez, Jesús
Bombardelli, Claudio
Lara, M.
Lucas, Fernando R.
Sanjurjo Rivo, Manuel
Curreli, D.
Lorenzini, Enrico C.
Scheeres, D.
Astronomy
Aeronautics
Numerical explorations show how the known periodic solutions of the Hill problem are modified in the case of the attitude-orbit coupling that may occur for large satellite structures. We focus on the case in which the elongation is the dominant satellite’s characteristic and find that a rotating structure may remain with its largest dimension in a plane parallel to the plane of the
primaries. In this case, the effect produced by the non-negligible physical length is dynamically
equivalent to the perturbation produced by an oblate central body on a mass-point satellite. Based
on this, it is demonstrated that the attitude-orbital coupling of a long enough body may change the
dynamical characteristics of a periodic orbit about the collinear Lagrangian points.
E.T.S.I. Aeronáuticos (UPM)
http://creativecommons.org/licenses/by-nc-nd/3.0/es/
2011-02-28
info:eu-repo/semantics/conferenceObject
Presentation at Congress or Conference
22nd International Symposium on Space Flight Dynamics - 22nd ISSFD | 22nd International Symposium on Space Flight Dynamics - 22nd ISSFD | 28/02/2011 - 04/03/2011 | Säo José dos Campos, Brasil
PeerReviewed
application/pdf
spa
info:eu-repo/semantics/openAccess
http://oa.upm.es/21139/