One of the challenges in modeling low-altitude mission scenarios at small bodies is the need to minimize the computation time penalty for more detailed shape models, especially when the scale of the detail is on the order of the spacecraft trajectory. This paper describes variants of the polyhedral model and their relative performance.
Augmentations to the polyhedral gravity model to facilitate small body navigations
2005-01-01
Preprint
No indication
English
Augmentations to the Polyhedral Gravity Model to Facilitate Small Body Navigation (AAS 05-146)
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