Long-term dynamics of fast rotating tethers around planetary satellites


Autoria(s): Urrutxua Cereijo, Hodei; Pelaez Alvarez, Jesus; Lara, Martín
Data(s)

2014

Resumo

We derive a semi-analytic formulation that enables the study of the long-term dynamics of fast-rotating inert tethers around planetary satellites. These equations take into account the coupling between the translational and rotational motion, which has a non-negligible impact on the dynamics, as the orbital motion of the tether center of mass strongly depends on the tether plane of rotation and its spin rate, and vice-versa. We use these governing equations to explore the effects of this coupling on the dynamics, the lifetime of frozen orbits and the precession of the plane of rotation of the tether.

Formato

application/pdf

Identificador

http://oa.upm.es/36913/

Idioma(s)

eng

Publicador

E.T.S.I. Aeronáuticos (UPM)

Relação

http://oa.upm.es/36913/1/INVE_MEM_2014_196640.pdf

Direitos

http://creativecommons.org/licenses/by-nc-nd/3.0/es/

info:eu-repo/semantics/restrictedAccess

Fonte

SpaceFlight Mechanics 2014 | 24th SpaceFlight Mechanics Meeting | 26-30 Ene 2014 | Santa Fe, New Mexico (EEUU)

Palavras-Chave #Aeronáutica #Física
Tipo

info:eu-repo/semantics/conferenceObject

Ponencia en Congreso o Jornada

PeerReviewed