Path: SC/BasicOrbit
% Compute the period for an orbit. You specify the semi-major axis. The default central body is the Earth. Type Period for a demo -------------------------------------------------------------------------- Form: p = Period( a, mu ) -------------------------------------------------------------------------- ------ Inputs ------ a (1,:) Semi-major axis (inf for a parabola and negative for a hyperbola) mu (1,1) Gravitational parameter (default = Earth) ------- Outputs ------- p (1,:) Period (s) --------------------------------------------------------------------------
Common: Graphics/Plot2D
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