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New approach of orbit determination strategy to improve the Stardust dynamic models

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dc.contributor.author You, T.-H. en_US
dc.contributor.author Ellis, J. en_US
dc.contributor.author McElrath, T. en_US
dc.date.accessioned 2004-09-23T21:40:29Z
dc.date.available 2004-09-23T21:40:29Z
dc.date.issued 2001-02-11 en_US
dc.identifier.citation 11th AAS/AIAA Space Flight Mechanics Meeting en_US
dc.identifier.citation Santa Barbara, California, USA en_US
dc.identifier.clearanceno 00-2024 en_US
dc.identifier.uri http://hdl.handle.net/2014/16118
dc.description.abstract This paper describes the estimation strategy to model the small forces, developed as a result of extensive analyses at Jet Propulsion Laboratory (JPL) and Lockheed Martin Astronautics (LMA). en_US
dc.format.extent 465296 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Stardust small force orbit determination spacecraft navigation en_US
dc.title New approach of orbit determination strategy to improve the Stardust dynamic models en_US


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