Calculation of the Hinge Moments of a Folding Wing Aircraft during the Flight-Folding Process

Table 1

Main parameters of the aircraft.

	c.g. coordinate, , , (m, m, m)	Inertia tensor, (kg m^2)
Unfolded	2.12, 0.00, 0.00	4502
Folded	2.12, 0.00, 0.24	4675