Pole Placement Method for Missile Control System Design

This paper designs a three-channel missile control system using the pole placement method, achieving the basic performance requirements. By selecting characteristic points for simulation during the vertical ascent and pitch phases, the system meets the attitude angle control requirements for vertical launch. The designed control law, however, shows limitations—demonstrating good performance initially but developing severe oscillations after a certain period. Alternative approaches or hybrid control methods could be explored to overcome these drawbacks and achieve more optimal results.