Research Article
Optimization of Trajectory Correction Scheme for Guided Mortar Projectiles
Table 2
Initial conditions and disturbances.
| Parameter | Unit | Mean value | Std. deviation |
| launching elevation angle | deg | 78.86 | 0.35 | Launching azimuth angle | deg | ā0.13 | 0.30 | Initial velocity | m/s | 280 | 3 | Wind | m/s | 0 | 2 |
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