Path: Orbit/Optimization
% This function is 3D orbit problem in equinoctial coordinates. It is designed to be called by ode113. -------------------------------------------------------------------------- Form: varargout = FLowThrust3D( t, x, flag, d ) -------------------------------------------------------------------------- ------ Inputs ------ t (1,1) Time x (13,1) States [p;f;g;h;k;L;m;lambda] flag (1,1) Flag from ode113 d (.) Structure to pass to the integration RHS ------- Outputs ------- xDot (13,1) State derivatives d[r;u;v;lambdaR;lambdaU;lambdaV;v/r]/dt or vnew (1,1) Value of constraint isterminal (1,1) 1 if a terminal constraint direction (1,1) Direction --------------------------------------------------------------------------
Sail: Optimization/ControlAngles3D Sail: OrbitDynamics/RHSEquinoctial
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