Rapid Ascent Trajectory Replanning with Customized Interior-Point Methods for Thrust Failure

The dataset was generated by customized interior-point solver.The dataset named "Parameter.mat" contains the simulation parameters of the target launch vehicle.The datasets named "Phase*" contain the thrust failure time and degree happened during the different phases. trajectories generated by the solver is also contained in these databases.The files named "Original Traj" contains the normal trajectory of the launch vehicle.