Research Article

Intelligent Controller Design for Quad-Rotor Stabilization in Presence of Parameter Variations

Table 1

Quadrotor parameters.

Symbol Quantity Value

Thrust factor N⋅S2
Drag coefficient N⋅m⋅s2
Moment of inertia along direction kg⋅m2
Moment of inertia along direction kg⋅m2
Moment of inertia along direction kg⋅m2
Center distance between the gravity of quadrotor and each propeller 0.1785 m
Total mass of the quadrotor 0.450 kg
Rotor inertia kg⋅m2
Gravity m/s2