Path: Orbit/OrbitMechanics
% Computes the sphere of influence ratio Computes the ratio of the sphere of influence to the distance between two bodies. Uses 2/5 power based on the argument due to Lagrange. m M ?-------------------------? |<---------- 1 ---------->| |----->| rOR -------------------------------------------------------------------------- Form: rOR = SphOI( m, M ) -------------------------------------------------------------------------- ------ Inputs ------ m (1,n) Mass of planet of interest M (1,m) Mass of other planet ------- Outputs ------- rOR (n,m) Ratio of sphere of influence for m to distance between the two planets -------------------------------------------------------------------------- References: Wiesel, W. E., Spaceflight Dynamics, McGraw-Hill, 1988, pp. 288-291. --------------------------------------------------------------------------
Common: Database/Constant Common: Graphics/Mesh2 Math: Linear/DupVect
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