Research Article
Fault-Tolerant Guidance of Rocket Vertical Landing Phase Based on MPC Framework
Table 5
Landing errors and masses under the condition that thrust cannot change continuously.
| | Landing position error/m | Landing velocity error/(m/s) | Landing mass/kg |
| Trajectory optimization | 407.6401 | 4.8062 | 23081.57 | Guidance | 0.0914 | 0.3145 | 23136.54 |
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