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Displacement of the Lagrange Equilibrium Points in the Restricted Three Body Problem With Rigid Body Satellite

Published online by Cambridge University Press:  12 April 2016

W.J. Robinson
W.J. Robinson*
Affiliation:
University of Bradford

Abstract

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In the restricted problem of three point masses, the positions of the equilibrium points are well known and are tabulated. When the satellite is a rigid body, these values no longer correspond to the equilibrium points. This paper seeks to determine the magnitudes of the discrepancies.

Type
Part V. Gravitational Problem of three or more bodies
Information
International Astronomical Union Colloquium , Volume 41: Dynamics of Planets and Satellites and Theories of their Motion , 1978 , pp. 305 - 314
Copyright
Copyright © Reidel 1978

References

Robinson, W.J.: 1974, Celes. Mech. 10, 17.CrossRefGoogle Scholar
Szebehely, V.: 1967, Theory of Orbits, Academic Press, New York and London.Google Scholar