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Enhancing the Cassini mission through FP applications after launch

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dc.contributor.author Morgan, Paula S.
dc.date.accessioned 2017-07-26T16:23:47Z
dc.date.available 2017-07-26T16:23:47Z
dc.date.issued 2016-03-05
dc.identifier.citation 2016 IEEE Aerospace Conference, Big Sky, Montana, March 5-12, 2016 en_US
dc.identifier.clearanceno 15-5556
dc.identifier.uri http://hdl.handle.net/2014/45786
dc.description.abstract This paper details the FP applications used to resolve the above issues as well as to optimize solutions for several other problems experienced by the Cassini spacecraft during its flight, in order to enhance the spacecraft's overall mission success throughout the 18 years of its 20 year expedition to and within the Saturnian system. en_US
dc.description.sponsorship NASA/JPL en_US
dc.language.iso en_US en_US
dc.publisher Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2016 en_US
dc.subject fault protection en_US
dc.title Enhancing the Cassini mission through FP applications after launch en_US
dc.type Presentation en_US


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