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Flyby Design Using Heteroclinic and Homoclinic Connections of Unstable Resonant OrbitsTour designs using flybys have traditionally been studied using two-body patched conic methods. Previous work has shown that trajectories designed using these techniques and with optimization methods follow the invariant manifolds of unstable resonant orbits as they transition between resonances. This work is continued here by computing heteroclinic and homoclinic trajectories associated with these unstable resonant orbits. These trajectories are used with multiple resonances to design flybys that transition between these resonances in the circular restricted three-body problem without the need for two-body approximations.
Document ID
20120002936
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Anderson, Rodney L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Lo, Martin W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 25, 2013
Publication Date
February 13, 2011
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AAS11-125
Meeting Information
Meeting: 21st AAS/AIAA Space Flight Mechanics Meeting
Location: New Orleans, LA
Country: United States
Start Date: February 13, 2011
End Date: February 17, 2011
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronautical Society
Distribution Limits
Public
Copyright
Other
Keywords
three body problem
homoclinic connection
resonant orbit
gravity assist
flyby heteroclinic connection

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