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. | |
Internacional
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Si |
JCR del ISI
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No |
Título de la revista
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Advances in the Astronautical Sciences |
ISSN
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1081-6003 |
Factor de impacto JCR
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Información de impacto
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Volumen
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155 |
DOI
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Número de revista
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Desde la página
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3257 |
Hasta la página
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3274 |
Mes
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SIN MES |
Ranking
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