Missile IGC Based on Improved Model Predictive Control and Sliding Mode Observer

Figure 5

Simulation results under Case 1: (a) intercept trajectory, (b) the LOS angular rate, (c) the attack angle, (d) the pitch angle, (e) the deflection angle, and (f) real value and estimate value of disturbance.

(a)

(b)

(c)

(d)

(e)

(f)