Intelligent guided missile

Guided missiles involve the use of conventional algorithms like proportional navigation algorithm and its variants which is optimal when the speed advantage of guided missile is very high and the maneuvering capability of the target is low. When the traditional navigational algorithm is pitched against the present fifth generation aircrafts which employ flyby-wire technology for high maneuverability and added with speeds between Mach-2 and Mach-3, the system´s efficiency drastically decreases. The missile needs to have a much higher speed advantage or to use a combination of artificial intelligence and modern control algorithms. Techniques to keep the guided missile airborne and results of pursuit and evasion with an autonomous intelligent agent incorporated in the control loop is presented.