Path: Missions/LunarLanding
% Equality constraints for the landing for a 2D flat planet problem. The constraint is the terminal altitude and velocities. They must be zero. The function integrates the trajectory to find the values. -------------------------------------------------------------------------- Form: [cIn, cEq, s, t] = LandingConst3D( x, d ) -------------------------------------------------------------------------- ------ Inputs ------ x (:,1) [beta;dT] d (.) Data structure describing spacecraft model ------- Outputs ------- cIn (1,1) Inequality contraints cEq (3,1) Equality constraints s (4,:) State t (1,:) Corresponding times --------------------------------------------------------------------------
Math: Integration/RK4 Math: Linear/Mag
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