NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Use of Invariant Manifolds for Transfers Between Three-Body SystemsThe Lunar L1 and L2 libration points have been proposed as gateways granting inexpensive access to interplanetary space. To date, only individual solutions to the transfer between three-body systems have been found. The methodology to solve the problem for arbitrary three-body systems and entire families of orbits does not exist. This paper presents the initial approaches to solve the general problem for single and multiple impulse transfers. Two different methods of representing and storing 7-dimensional invariant manifold data are presented. Some particular solutions are presented for the transfer problem, though the emphasis is on developing methodology for solving the general problem.
Document ID
20040015252
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Beckman, Mark
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Howell, Kathleen
(Purdue Univ. IN, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2003
Subject Category
Lunar And Planetary Science And Exploration
Meeting Information
Meeting: 2004 AAS/AIAA Space Flight Mechanics
Location: Maui, HI
Country: United States
Start Date: February 9, 2004
Sponsors: American Astronomical Society, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available