------------------------------------------------------------------------------- Computes a collinear Lagrange point. Default is for the earth/moon system. ------------------------------------------------------------------------------- Form: rL = RLagrange( rS, mR, lPoint ) ------------------------------------------------------------------------------- ------ Inputs ------ rS (3,1) R of the secondary mR (1,1) Mass secondary/mass primary lPoint (1,1) Desired Lagrange point ------- Outputs ------- rL (3,1) Lagrange coordinates -------------------------------------------------------------------------------