Examining the Stability and Control of Wheel Channel in Missile by Self-Regulatory Controller

In this paper the stability of the wheel channel or Roll of missile, which has been the focus of attention of scientist for a long time has been investigated. First, its stability has been studied through Liapanove Stability. Then the visibility and controllability of it have been examined. In order to have access to the missile, the special model has been considered. In order to obtain self regulatory gains, which has been the subject of the current research, LQR method which is a linear estimation has been used. An estimation with order 2 can prepare the regulator for simulation process.