Optimization calculation about control force of trajectory corrected projectile

In this paper, trajectory correction of canard control anti-aircraft shells is researched. After launch, once targets make circumvent flight, we must adjust projectile control force to correct ballistic. Projectile free flying model and control flying model are established. Target Initial flying model and maneuvering flying model are assumed. According to the models of projectile and target, appropriate optimizing algorithm is selected, control force of projectile is optimizing calculated. We can draw the conclusion that the optimization algorithm is feasible.