Published 2001
| Accepted Version
Book Section - Chapter
Open
Invariant Manifolds, the Spatial Three-Body Problem and Space Mission Design
Chicago
Abstract
The invariant manifold structures of the collinear libration points for the spatial restricted three-body problem provide the framework for understanding complex dynamical phenomena from a geometric point of view. In particular, the stable and unstable invariant manifold \tubes" associated to libration point orbits are the phase space structures that provide a conduit for orbits between primary bodies for separate three-body systems. These invariant manifold tubes can be used to construct new spacecraft trajectories, such as a \Petit Grand Tour" of the moons of Jupiter. Previous work focused on the planar circular restricted three-body problem. The current work extends the results to the spatial case.
Additional Information
© 2002 Published for the American Astronautical Society by Univelt. We would like to thank Steve Wiggins, Laurent Wiesenfeld, Charles Jaffé, T. Uzer and Luz Vela-Arevalo for their discussions. This work was carried out in part at the Jet Propulsion Laboratory and the California Institute of Technology under a contract with the National Aeronautics and Space Administration. In addition, the work was partially supported by the NSF grant KDI/ATM-9873133, JPL's LTool project, AFOSR Microsat contract F49620-99-1-0190 and Catalan grant 2000SGR-00027.Attached Files
Accepted Version - GoKoLoMaMaRo2001.pdf
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Additional details
- Eprint ID
- 20327
- Resolver ID
- CaltechAUTHORS:20101007-081509793
- NSF
- KDI/ATM-9873133
- JPL LTool project
- Air Force Office of Scientific Research (AFOSR) Microsat
- F49620-99-1-0190
- Catalan
- 2000SGR-00027
- Created
-
2010-11-19Created from EPrint's datestamp field
- Updated
-
2019-10-03Created from EPrint's last_modified field
- Series Name
- Advances in Astronautical Sciences
- Series Volume or Issue Number
- 109