SIMULATION OF GUIDED MISSILE TRAJECTORIES FOR TARGET -INTERCEPTION

Abstract

The prime concern of this dissertation is centered on the trajectories corresponding the navigational homing systems and their related problem especially the interception of target with a missile belonging to this family. The trajectories of a guided missile are simulated for target interception using guidance laws. For the change in missile and target parameters like velocity, position, target heading angle, trajectories are computed. In addition the linearization of proportional law, which is the general law, is also discussed. The display and computational work has been carried out and implemented mainly . using object oriented programming approach C + + to understand such interception problem more closely. The study of missile system related instruments and propulsion is also carried out in order to understand limitation of missiles in real life.