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The role of invariant manifolds in lowthrust trajectory design (part III)This paper is the third in a series to explore the role of invariant manifolds in the design of low thrust trajectories. In previous papers, we analyzed an impulsive thrust resonant gravity assist flyby trajectory to capture into Europa orbit using the invariant manifolds of unstable resonant periodic orbits and libration orbits. The energy savings provided by the gravity assist may be interpreted dynamically as the result of a finite number of intersecting invariant manifolds. In this paper we demonstrate that the same dynamics is at work for low thrust trajectories with resonant flybys and low energy capture. However, in this case, the flybys and capture are effected by continuous families of intersecting invariant manifolds.
Document ID
20060043720
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Lo, Martin W.
Anderson, Rodney L.
Lam, Try
Whiffen, Greg
Date Acquired
August 23, 2013
Publication Date
January 22, 2006
Subject Category
Astrodynamics
Report/Patent Number
AAS 06-190
Meeting Information
Meeting: AIAA/AAS Astrodynamics Specialist Conference
Location: Tampa, FL
Country: United States
Start Date: January 22, 2006
End Date: January 26, 2006
Distribution Limits
Public
Copyright
Other
Keywords
low thrust trajectories
three-body problems
Jupiter Icy Moons Orbiter (JIMO)
invariant manifolds

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