Stability Characteristics of Wing Span and Sweep Morphing for Small Unmanned Air Vehicle: A Mathematical Analysis

Table 1

Model parameters.

Parameter name	Value
Wingspan	1.00 m
Wing chord	0.24 m
Wing area	0.24 m^2
Aspect ratio	4.17
Taper ratio	1.0
Wing sweep (˄)	0°
Wing dihedral	0°
Wing LE position	(0.12, 0, 0) m
Wing, elevator airfoil	NACA 0012
Fuselage length	0.84 m
Elevator LE position	(0.7, 0, 0.01) m
Elevator root chord	0.14 m
Elevator tip chord	0.1 m
Elevator area	0.05 m^2
Vertical fin area	0.02 m^2
Tail volume	0.054
Total mass	0.495 kg
Center of gravity	(0.2, 0, 0.1) m