Research on Aircraft Attitude Control Method Based on Linear Active Disturbance Rejection

Table 1

Aircraft parameter.

Parameters	Numerical value
	19000 kg
	3900 kg.m^2
	393600 kg.m^2
	393600 kg.m^2
	39900 pa
	19 m
	1.1 m^2
	3°
	3°
	62°
	0°
	0°
	0°
	0°
	0°
	65°
	0°
	0°
	0°