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

Figure 8

3D view (left column) and Casimir power (right column) of system (15) with (a, b) , (c, d) , (e, f) , and (g, h) .

(a)

(b)

(c)

(d)

(e)

(f)

(g)

(h)