Missile guidance systems consist of various methods to direct the missile to its intended target. This device is used to steer a missile toward its target and it highly depends on the network, and disruption from a guidance system intrusion throws the missile off-course and even disrupts its trajectory. Each missile guidance system consists of a flight path control system and an attitude control system. Attitude control systems are responsible for maintaining a desired attitude on a given trajectory by controlling the pitch, roll, and yaw of the missile.