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Dynamics About Uniformly Rotating Tri-Axial Ellipsoids. Application to Dynamics About AsteroidsThe general problem of satellite and particle dynamics about a uniformly rotating tri-axial ellipsoid with constant density is formulated.
Document ID
20060038345
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
hdl:2014/33865
Authors
Scheeres, D. J.
Date Acquired
August 23, 2013
Publication Date
January 1, 1994
Subject Category
Lunar And Planetary Science And Exploration
Distribution Limits
Public
Copyright
Other
Keywords
satellite dynamics particle dynamics ellipsoids asteroid dynamics

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