Path: Orbit/OrbitPropagator
% The aero force model. This is a pure drag model. -------------------------------------------------------------------------- Form: x = FAero( action, modifier, u, t ) -------------------------------------------------------------------------- ------ Inputs ------ action (1,:) Action 'initialize', 'update' modifier (1,:) Modifier to the action or data structure if initialization u (7,1) [v;rho] [km/sec;kg/m^3] t (1,1) Time ------- Outputs ------- x (3,1) Force vector in the v frame (kg-km/sec^2) --------------------------------------------------------------------------
ACPro: Help/HelpSystem Common: General/CloseFigure Math: Linear/Mag Orbit: OrbitPropagator/PropagateOrbitPlugIn
Back to the Orbit Module page