Integrated Guidance and Control Design of Rolling-Guided Projectile Based on Adaptive Fuzzy Control with Multiple Constraints

Figure 3

Experimental curves of operating condition 1. (a) Trajectory of projectile and target. (b) Normal overload. (c) Quasi-attack angle. (d) Equal pitch canard angle. (e) Pitch canard angle. (f) LOS inclination angle rate. (g) Pitch angle. (h) and disturbance . (i) and disturbance .

(a)

(b)

(c)

(d)

(e)

(f)

(g)

(h)

(i)