Path: SC/Ephem
% Computes the position and velocity of stable Lagrange points.
Assumes thes positive x axis in the rotating frame is towards the moon
from the Earth.
See also LagrangePointsL1ToL5 and MoonV1.
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Form:
[r, v, mLEToECI] = TransformLagrangePoints( p, jD )
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Inputs
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p (2,:) Points
jD (1,1) Date of interest
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Outputs
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r (3,1) Position of stable point in ECI frame
v (3,1) Velocity of stable point in ECI frame
mLEToECI (3,3) Transformation matrix from Lunar-Earth to ECI
frame
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