BTT Missile Kinematic Decoupling with Dynamic Performance Compensation

The BTT missile exists strong kinematical coupling,decoupling method with directly lead into angular rate compensation is not satisfactory for engineering. The body dynamic performance is considered which impact on the control system,the differential-integral form of decoupling is introduced to compensate body dynamic characteristics,for BTT missile autopilot kinematics decoupling design. Simulation example validates correctness of decoupled design,the final pull side simulation assess its robustness,its effectiveness is proved.