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%