Path: Orbit/RHSOrbit
% Orbit equations for InterstellarSim. Since version 2. -------------------------------------------------------------------------- Form: [xDot, thrust, power] = FHel( x, t, d ) -------------------------------------------------------------------------- ------ Inputs ------ x (5,1) The state vector [x;y;xDot;yDot;m] t Time d (:) Data structure ------- Outputs ------- xDot (5,1) The derivative of the state vector thrust (1,1) The thrust power (1,1) The available power --------------------------------------------------------------------------
Back to the Orbit Module page