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

Antreasian, P. G.; Chesley,  S. R.; Miller,  J. K.; Bordi,  J. J.; Williams,  B. G.

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