Design of LPV-Based Sliding Mode Controller with Finite Time Convergence for a Morphing Aircraft

Table 1

b	0.3 m
Λ	0~45 deg
Δ	0~2 m
Jy	3107.53 kg⋅m^2
l1	2.5 m
l2	2.0 m
mb	771.79 kg
m1	54 kg
m2	13.605 kg
	129.27 N/%