Apply the z transform methodology to sampled data systems to implement control strategies for computer control.
Employ computer tools in system modeling and design, e.g MATLAB, Simulink
The missile system in figure 1 can be aerodynamically controlled by torque created by the deflection of control surfaces on the missile’s body. The command to deflect these control surfaces come from a computer that uses tracking data along with programmed guidance equations to determine whether the missile is on [login to view URL] information from the guidance equations is used to developed flight control commands for the missile. The simplified block diagram of the missile system is shown in figure 2.
Given the missile system has a transfer function