The elliptical three-body problem - Triangular solution

Details The elliptical three-body problem - Triangular solution The elliptical three-body problem - Triangular solution

Sep 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992an....313..315t&link_type=abstract

Astronomische Nachrichten (ISSN 0004-6337), vol. 313, no. 5, p. 315-317.

Astronomy and Astrophysics

Astronomy

1

Celestial Mechanics, Lagrangian Equilibrium Points, Three Body Problem, Eccentric Orbits, Triangles

Scientific paper

The restricted three-body with problem with an eccentric orbit is
reviewed and the positions of the triangular Lagrangian points are
determined. For a fixed value of the true anomaly the three bodies are
situated at the corners of an isosceles triangle.

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