Adaptive Super-Twisting Algorithm-Based Nonsingular Terminal Sliding Mode Guidance Law

Figure 2

Simulation results of Case 1. (a) Missile and target motion trajectory. (b) Relative distance between the missile and the target. (c) Sliding mode. (d) LOS angle. (e) LOS angular rate. (f) Missile overload.

(a)

(b)

(c)

(d)

(e)

(f)