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.

该数据集由定制化的内点求解器生成。名为“Parameter.mat”的数据集包含目标发射运载工具的模拟参数。以“Phase*”命名的数据集则记录了在不同阶段发生的推力故障时间和程度。由求解器生成的轨迹也包含在这些数据库中。名为“Original Traj”的文件则包含了发射运载工具的正常轨迹。