JPL Technical Report Server

Augmentations to the polyhedral gravity model to facilitate small body navigations

Show simple item record

dc.contributor.author Cangahuala, L. Alberto
dc.date.accessioned 2005-09-15T22:27:34Z
dc.date.available 2005-09-15T22:27:34Z
dc.date.issued 2005-01
dc.identifier.citation 2005 AAS/AIAA Spaceflight Mechanics Meeting en
dc.identifier.clearanceno 05-0170
dc.identifier.uri http://hdl.handle.net/2014/37527
dc.description.abstract 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. en
dc.description.sponsorship NASA en
dc.format.extent 187793 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2005. en
dc.subject small body orbits en
dc.subject gravity fields en
dc.title Augmentations to the polyhedral gravity model to facilitate small body navigations en
dc.type Preprint en


Files in this item

This item appears in the following Collection(s)

Show simple item record

Search


Browse

My Account