Research Article

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

Table 8

Landing errors and masses of the guidance method.

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

0.00350.023923230.63
4.162729.245623957.32
0.00350.023923230.63
4.162729.245623957.32