Path: SC/BasicOrbit
% Computes the right-hand-side of the orbit equations about a mass point. Only the first input is required. -------------------------------------------------------------------------- Form: xDot = FOrbCart( x, t, a, mu ) -------------------------------------------------------------------------- ------ Inputs ------ x (6,1) The state vector [r;v] t (1,1) Time (unused) a (3,1) External acceleration (default is zero) mu (1,1) Gravitational parameter (default is Earth) ------- Outputs ------- xDot (6,1) The derivative of the state vector --------------------------------------------------------------------------
Math: Linear/Mag
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