Descripción
|
|
---|---|
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. | |
Internacional
|
Si |
Nombre congreso
|
24th AAS/AIAA Space Flight Mechanics Meeting |
Tipo de participación
|
960 |
Lugar del congreso
|
Santa Fe, New Mexico (EEUU) |
Revisores
|
Si |
ISBN o ISSN
|
978-0-87703-611-1 |
DOI
|
|
Fecha inicio congreso
|
26/01/2014 |
Fecha fin congreso
|
30/01/2014 |
Desde la página
|
3423 |
Hasta la página
|
3442 |
Título de las actas
|
Advances in the Astronautical Sciences |