Trajectory tracking of a satellite communicated missile with Fuzzy and PID control

In this study, the trajectory of a satellite communicated missile, which is thrown from combat plane to combat plane, has been investigated with using Fuzzy and PID control separately. The Guidance Section of Missile consists of an active radar seeker and radome, radar altimeter and antennas, and power converter. Simulations have been done with Matlab Simulink toolbox and utilized standard transfer function of missile on block diagram. The results, enabled with PID and Fuzzy Control, have been compared and given in this study.