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SUPPORT SITE |
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Path: Orbit/OrbitCoord
% 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 --------------------------------------------------------------------------
Common: Database/Constant Common: General/IsVersionAfter Common: Time/Date2JD SC: Ephem/MoonV1
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