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(abstract) Maneuver Design for Galileo Asteroid FlybysThis paper will address the trajectory correction maneuvers (TCMs) which enabled the successful completion of the circuitous VEEGA trajectory while providing for the first ever encounters with main-belt asteroids.
Document ID
20060039619
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
hdl:2014/36481
Authors
Wilson, Michael G.
Potts, Christopher L.
Date Acquired
August 23, 2013
Publication Date
May 22, 1994
Subject Category
Astrodynamics
Distribution Limits
Public
Copyright
Other
Keywords
Galileo trajectory correction maneuvers Jupiter asteroids VEEGA trajectory

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