Physics
Scientific paper
Oct 1980
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1980cemec..22..241r&link_type=abstract
Celestial Mechanics, vol. 22, Oct. 1980, p. 241-253.
Physics
17
International Sun Earth Explorer 3, Lagrangian Equilibrium Points, Orbit Calculation, Orbital Mechanics, Satellite Orbits, Collinearity, Equations Of Motion, Libration, Three Dimensional Motion
Scientific paper
A third-order analytical solution for halo-type periodic motion about the collinear points of the circular-restricted problem is presented. The three-dimensional equations of motion are obtained by a Lagrangian formulation. The solution is constructed using the method of successive approximations in conjunction with a technique similar to the Lindstedt-Poincare method. The theory is applied to the sun-earth system.
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