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

Figure 12

Time series of QUAV characteristics for three different configurations: (a) angular velocity ; (b) roll angle ; (c) pitch angle ; (d) yaw angle ; (e) acceleration along the z-axis; (f) displacement along the z-axis.

(a)

(b)

(c)

(d)

(e)

(f)