Research Article

Fault-Tolerant Guidance of Rocket Vertical Landing Phase Based on MPC Framework

Table 7

Landing errors and masses of the trajectory optimization algorithm.

DeviationLanding position error/mLanding velocity error/(m/s)Landing mass/kg

289.59334.979023135.95
356.56896.259823135.95
289.95844.979023135.95
356.56896.259823135.95