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Descripción
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| 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 dimension is dynamically equivalent to the perturbation produced by an oblate central body on a masspoint 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. | |
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Internacional
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JCR del ISI
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No |
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Título de la revista
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Journal of Aerospace Engineering, Sciences and Applications |
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ISSN
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2236-577X |
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Factor de impacto JCR
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Información de impacto
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Volumen
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IV |
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DOI
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Número de revista
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1 |
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Desde la página
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73 |
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Hasta la página
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81 |
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Mes
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MARZO |
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Ranking
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