Modeling and Simulation of China C Series Large Aircraft with Microburst

Table 2

Parameters of aircraft.

Symbols	Value	Dimension	Illustration
	7310	Kg	Aircraft mass
	23.0	m^2	Reference area
	7.15	m	Wing span
	4.002	m	Mean aerodynamic chord
	450	Kg⋅m^2	Inertia moment around -axis
	4400	Kg⋅m^2	Inertia moment around -axis
	4700	Kg⋅m^2	Inertia moment around -axis
	85.37	Kg⋅m^2	Product of inertia