Research Article

Velocity Control for Coning Motion Missile System Using Direct Discretization Method

Table 1

Simulation results produced by different guidance laws.

Guidance with velocity controlGuidance without velocity controlOptimization trajectory profilePSO trajectory profile

Final velocity (m/s)254.09281.36255.0255.6
Final flying path angle (deg)−15.65−20.18−21.46−20.93
Miss distance (m)2.2 1.60.60.8