Research Article
Designing Backstepping Control System for Hypersonic Vehicle Based on Feedback Linearization
Table 4
The deflections and deflection values.
| Deflections | Deflection values |
| Lift | ±5% | Pitch moment | ±20% | Atmospheric density | ±5% | Rotary inertia | ±10% | Average aerodynamic airfoil chord length | ±10% | Total length of the flight vehicle | ±10% | Take-off gross weight | ±10% |
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