Evasion-Faced Fast Adaptive Neural Attitude Control for Generic Hypersonic Vehicles with Structural and Parametric Uncertainties

Table 4

The performance comparison of the three control methods.

	FANNC	MRAC	ANNC
Pitch channel	Maximal time delay 0.01	Maximal time delay 0.5	Maximal time delay 0.35
	Maximal tracking error 0.05	Maximal tracking error 0.6	Maximal tracking error 0.4
Yaw channel	Maximal time delay 0	Maximal time delay 0	Maximal time delay 0
	Maximal tracking error 0.005	Maximal tracking error 0.09	Maximal tracking error 0.36
Roll channel	Maximal time delay 0.02	Maximal time delay 0.4	Maximal time delay 0.45
	Maximal tracking error 0.05	Maximal tracking error 0.95	Maximal tracking error 0.8