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Execution-error modeling and analysis of the Cassini-Huygens spacecraft through 2007

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dc.contributor.author Wagner, Sean V.
dc.contributor.author Goodson, Troy D.
dc.date.accessioned 2011-01-28T17:53:40Z
dc.date.available 2011-01-28T17:53:40Z
dc.date.issued 2008-01-27
dc.identifier.citation Spaceflight mechanics 2008 : proceedings of the AAS/AIAA Space Flight Mechanics Meeting held January 27-31, 2008, Galveston, Texas en_US
dc.identifier.clearanceno 08-0089
dc.identifier.uri http://hdl.handle.net/2014/41690
dc.description.abstract The Cassini-Huygens spacecraft arrived at Saturn in 2004, beginning a four-year tour. Much of mission’s continued success at Saturn can be attributed to the excellent performance of the propulsion systems and attitude control. In order to better understand this performance, the Cassini Navigation Team has continued to analyze and refine the execution-error models for the propulsion systems. This paper documents the evolution of the execution-error models employed for maneuvers, along with the analysis, procedures, and software associated with the model development. en_US
dc.description.sponsorship AAS/AIAA en_US
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2008. en_US
dc.subject Cassini-Huygens spacecraft en_US
dc.subject spacecraft performance en_US
dc.subject execution-error models en_US
dc.subject propulsion systems en_US
dc.title Execution-error modeling and analysis of the Cassini-Huygens spacecraft through 2007 en_US
dc.type Preprint en_US


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