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The design and navigation of the NEAR-Shoemaker landing on Eros

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dc.contributor.author Antreasian, P. G. en_US
dc.contributor.author Chesley, S. R. en_US
dc.contributor.author Miller, J. K. en_US
dc.contributor.author Bordi, J. J. en_US
dc.contributor.author Williams, B. G. en_US
dc.date.accessioned 2004-09-22T23:49:46Z
dc.date.available 2004-09-22T23:49:46Z
dc.date.issued 2001-07-30 en_US
dc.identifier.citation AAS/AIAA Astrodynamics Specialist Conference en_US
dc.identifier.citation Quebec City, Quebec, Canada en_US
dc.identifier.clearanceno 01-1393 en_US
dc.identifier.uri http://hdl.handle.net/2014/12977
dc.description.abstract This paper discusses the design, navigation and the Monte Carlo error analyses that were critical to the design of this landing scenario. Also described is the reconstruction of the landing trajectory using radio metric, optical landmark and laser ranging tracking data, which determined the characteristics of the landing to be well within the error analyses. en_US
dc.format.extent 1156083 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other NEAR asteroids landing polyhedral gravity Eros navigation en_US
dc.title The design and navigation of the NEAR-Shoemaker landing on Eros en_US


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