Effects of Wind Disturbance on the Aerodynamic Performance of a Quadrotor MAV during Hovering

Table 1

Rotor parameters.

Radius (m)	Blade pitch (m)	Twist (deg)	RPM^1 (RPM)	Reynolds number (10^5)	Max camber (%)	Mach number (-)
0.2	0.157	0	1500~2300	0.75~1.25	5.5	0.1~0.15

¹RPM: Revolutions Per Minute.