Influence of Revolving Angle Measure Precision and Actuator Performance on Control Force

A control mathematical model in pitch and yaw direction is presented to apply on missiles controlled by double-channel with style canard. Based on the mathematical model, the influence of deflection angle measurement error and actuator performance on actuator control is analyzed. The results show that the measure error of lean angle and actuator delay will produce control coupling in pitch and yaw direction and that will reduce control efficiency.