Sign Stability for Switched Linear Systems and Its Application in Flight Control

Figure 3

Time histories of system states and control inputs under perturbations: (a) angle of attack, (b) pitch rate, (c) pitch angle, (d) elevator, (e) elevon, (f) canard, and (g) symmetric aileron.

(a)

(b)

(c)

(d)

(e)

(f)

(g)