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Descripción
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| There are many asteroids for which the attitude coupling imposes harsh demands to the numerical propagation of their dynamics. Special regularization methods are appropriate to overcome such difficulties, where perturbations techniques make their best. The perturbation techniques used to derive the DROMO regularization method for orbital dynamics, have now been extended to the attitude dynamics problem with equally remarkable results both in terms of speed and accuracy. The combination of these DROMO-based techniques is thus appropriate for the propagation of strongly coupled bodies. | |
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Internacional
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Si |
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Nombre congreso
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25th AAS/AIAA Spaceflight Mechanics Meeting |
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Tipo de participación
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960 |
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Lugar del congreso
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Williamsburg, Virginia |
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Revisores
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Si |
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ISBN o ISSN
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1081-6003 |
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DOI
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Fecha inicio congreso
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11/01/2015 |
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Fecha fin congreso
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15/01/2015 |
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Desde la página
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1 |
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Hasta la página
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18 |
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Título de las actas
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Advances in the Astronautical Sciences |