Wind and Payload Disturbance Rejection Control Based on Adaptive Neural Estimators: Application on Quadrotors

Table 1

Parameter values of the model.

Parameter	Description	Value/Units
	Longitude of an arm	0.232 m
	Mass of the quadrotor	0.52 Kg
	Drag coefficient	7.5e^−7 N.m.s^2
	Thrust coefficient	3.13e^−5 N.s^2
	Inertia in X	6.228e^−3 Kg.m^2
	Inertia in Y	6.225e^−3 Kg.m^2
	Inertia in Z	1.121e^−2 Kg.m^2
	Density of the air	1.2 Kg/m^3
	Area in the direction of the wind	0.0186 m^2
	Wind drag coefficient	1