Path: SC/Ephem
% Computes the position of Lagrange points in normalized rotating
coordinates with the origin at the joint center-of-mass.
For a demo of the Earth Moon system type LagrangePointsL1ToL5
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Form:
p = LagrangePointsL1ToL5( mu )
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Inputs
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mu (1,1) Ratio of smaller mass to total mass
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Outputs
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p (2,5) [L1, L2, L3, L4, L5]
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Reference: Szebehely, V., "Theory of Orbits", Academic Press, 1967,
pp. 134-138.
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