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In flight estimations of Cassini spacecraft inertia tensor and thruster magnitude

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dc.contributor.author Feldman, Antonette
dc.contributor.author Lee, Allan Y.
dc.date.accessioned 2006-05-01T20:29:08Z
dc.date.available 2006-05-01T20:29:08Z
dc.date.issued 2006-01-23
dc.identifier.citation AIAA/AAS Space Flight Mechanics Conference, Tampa, Florida, January 23-25, 2006. en
dc.identifier.clearanceno 06-0127
dc.identifier.uri http://hdl.handle.net/2014/39202
dc.description.abstract This paper describes two methods used by the Cassini Attitude Control team to determine these key parameters and how flight telemetry was used to estimate them. The method for estimating the spacecraft inertia tensor exploits the conservation of angular momentum during spacecraft slews under reaction wheel control. en
dc.description.sponsorship NASA/JPL en
dc.format.extent 265771 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2006. en
dc.subject Cassini en
dc.subject inertia properties en
dc.subject thruster en
dc.title In flight estimations of Cassini spacecraft inertia tensor and thruster magnitude en
dc.type Preprint en


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