Research Article
Firing Control Optimization of Impulse Thrusters for Trajectory Correction Projectiles
Table 1
Initial conditions and disturbances.
| Parameter | Unit | Mean value | Standard deviation |
| Launching elevation angle | deg | 42.51 | 0.2 | Launching azimuth angle | deg | 0.1 | 0.2 | Impulse of the main rocket motor | % | 100 | 0.1 | Wind | m/s | 0 | 2 |
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