Path: Missions/MarsOrbiter
% Right hand side for a Mars orbit simulation. -------------------------------------------------------------------------- Forms: xDot = RHSMarsOrbit( x, ~, mu ) -------------------------------------------------------------------------- ------ Inputs ------ x (:,1) State [rECI;vECI;...] t (1,1) Time (not used) mu (1,1) Gravitational constant ------- Outputs ------- xDot (:,1) dx/dt --------------------------------------------------------------------------
Math: Linear/Mag
Back to the Missions Module page