A L₁ Adaptive Control Scheme for UAV Carrier Landing Using Nonlinear Dynamic Inversion

Table 1

Summary of EQ model physical parameters.

Parameter	Value
Weight	kg
Wing area	75.12 m^2
Mean aerodynamic chord	5.68 m
Wing span	16.67 m
Aspect ratio	3.70
	kg·m^2
	kg·m^2
	kg·m^2
	0.00 kg·m^2