Modeling and Analysis of Chaos and Bifurcations for the Attitude System of a Quadrotor Unmanned Aerial Vehicle

Table 2

Parameter values of the quadrotor [3, 8].

Parameter	Value
(m/s^2)	9.81
(kg)	0.468
(m)	0.225
(N·m/rad/s)	2.9e − 5
(m)	1.1e − 6
(kg·m^2)	3.4e − 5
Ix (kg·m^2)	4.9e − 3
Iy (kg·m^2)	9.8e − 3
Iz (kg·m^2)	8.8e − 3
(N/m/s)	2.45e − 4
(N/m/s)	8.82e − 4
(N/m/s)	4.40e − 4
(N/rad/s)	2.45e − 4
(N/rad/s)	8.82e − 4
(N/rad/s)	4.40e − 4