Robust Design of Stochastic Controller for a Guidance System of Command Guided Missile

In this work, we use the previous results on the stabilizing property of a control scheme designed for a class of continuous time linear system with additive noise. The existing controller will be made more robust with a prescribed degree of stability by proper modifications. A state feedback controller is used in order to minimize the error between a reference states, which are the states of the system when there is no noise, and the system states which are affected by the noise. this noise is represented by a white noise with zero mean and unit variance.