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Notes on the restricted three body problem- approximate behavior of solutions near the collinear lagrangian pointsStudies the solutions of the restricted three-body problem near those equilibrium points which are collinear with the two positive masses. This is done to gain insight toward the development of an analytic proof and classification of the periodic orbits that pass near these equilibrium points, which have been discovered numerically by M. Davidson, and also to hopefully gain insight into the nature of solutions of the restricted three-body problem in general. The qualitative observations that are made are all deduced from the linearized equations.
Document ID
19650023457
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Technical Report
Authors
C C Conley
(University of Wisconsin–Madison Madison, Wisconsin, United States)
Date Acquired
August 2, 2013
Publication Date
July 12, 1965
Publication Information
Publication: Progress Report No. 7 on Studies in the fields of Spaceflight and Guidance Theory
Publisher: National Aeronautics and Space Administration
Subject Category
Astrodynamics
Report/Patent Number
NASA-TM-X-53292
Accession Number
65N33058
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Approximation method
Lagrange coordinate
Jacobi Integral
Three-body problem
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