2026-10-15T02:02:04Z https://www.scidb.cn/oai

10.57760/sciencedb.01681 2022-04-08T09:07:41Z

2022-04-08 Rapid Ascent Trajectory Replanning with Customized Interior-Point Methods for Thrust Failure doi:10.57760/sciencedb.01681 en 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. Trajectory optimization; Real-time onboard optimization; Customized interior-point methods; Thrust failure problem; Online orbit estimation Kai Chen PUBLIC https://creativecommons.org/licenses/by/4.0/ dataset Science Data Bank