Full-State-Constrained Adaptive Control for a Class of UAVs Suffering from Coupled Uncertainties Using the HOBLF

Table 2

The initial values of the system states.

Variable	Implication	Value
	Pitch angle	0.2
	Yaw angle	0.1
	Roll angle	0.1
	Pitch rate	0
	Yaw rate	0
	Roll rate	0
	Adaptive parameter	0.001
	Gain of the adaptive law	1, 2
	Other parameters of the adaptive law	5