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Descripción
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| For long enough tethers, the coupling of the attitude and orbital dynamics may show non-negligible effects in the orbital motion of a tethered satellite about a central body. In the case of fast rotating tethers the attitude remains constant, on average, up to second order effects. Besides, for a tether rotating in a plane parallel to the equatorial plane of the central body, the attitude?orbit coupling effect is formally equal to the perturbation of the Keplerian motion produced by the oblateness of the central body and, therefore, may have a stabilizing effect in the orbital dynamics. In the case of a tethered satellite in a low lunar orbit, it is demonstrated that feasible tether lengths can help in modifying the actual map of lunar frozen orbits | |
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Internacional
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Si |
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JCR del ISI
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Si |
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Título de la revista
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Acta Astronautica |
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ISSN
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0094-5765 |
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Factor de impacto JCR
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Información de impacto
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Volumen
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79 |
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DOI
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Número de revista
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Desde la página
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52 |
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Hasta la página
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60 |
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Mes
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NOVIEMBRE |
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Ranking
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