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A global solution for the gravity field, rotation, landmarks and ephemeris of ErosThis solution uses the entire one-year in orbit collection of X-band radiometric tracking (Doppler and range) from the Deep Space Network and landmark tracking observations generated from the NEAR spacecraft images of Eros.
Document ID
20060032096
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/13541
Authors
Konopliv, A. S.
Miller, J. K.
Owen, W. M.
Yeomans, D. K.
Giorgini, J. D.
Garmier, R.
Barriot, J. P.
Date Acquired
August 23, 2013
Publication Date
December 3, 2001
Subject Category
Lunar And Planetary Science And Exploration
Distribution Limits
Public
Copyright
Other
Keywords
asteroid Eros gravity NEAR small bodies orbit determination

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