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SUPPORT SITE |
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SUPPORT SITE |
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Path: Orbit/OrbitCoord
% Computes the semi major axis from apogee and perigee radii -------------------------------------------------------------------------- Form: a = RARP2A( rA, rP ) -------------------------------------------------------------------------- ------ Inputs ------ rA (1,m) Apogee radius rP (1,n) Perigee radius ------- Outputs ------- a (m,n) Semi major Axis --------------------------------------------------------------------------
Common: Graphics/Mesh2 Math: Linear/DupVect
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