Research Article
Study on Initial Disturbance of Airborne Missile’s Horizontal Backward Derailment under Continuous Gust
| Parameter | Value |
| Flight altitude (m) | 8000 | Flight speed (m/s) | 80 | Air density (kg/m3) | 0.54 | Aircraft weight (kg) | 271632 | Pitch moment of inertia (kg/m2) | |
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