Designing Backstepping Control System for Hypersonic Vehicle Based on Feedback Linearization

Table 1

The main technical parameters of CSULA-GHV.

Name	Number	Unit
Reference area	33.4118	m^2
Average aerodynamic airfoil chord length	33.3770	m
Take-off gross weight	5000	kg
Rotary inertia	460590	kg⋅m^2
Velocity	3018	m/s
Altitude	30000	m