Design of Guidance and Control Systems for Tactical Missiles

Accelerometers Kalman Filter Aerodynamic Configuration Aerodynamic Transfer Functions as Controlled Plant Aerodynamic Derivatives Acceleration Command Autopilot Design autopilot designs Control Surface Conventions Bode Diagram Flight Path Angle Guidance Law Guidance Loop Guidance Radar Control Loop Disturbance Moment Euler Equations of Motion Lower Static Stability Missile Body Miss Distance missile guidance control systems Gimbal Angle Guidance Dynamics Pitch/Yaw Attitude Autopilot Optimal Guidance Law Guidance Radar Pi Compensator Real Seeker Model Receiver Thermal Noise Roll Angular Velocity Scale-factor error model Proportional Navigation Guidance Target Maneuvering Acceleration Estimation seeker system designs Trajectory Models Integrated GNSS Components Three-loop autopilot Missile Control Methods Yaw Angular Velocity Proportional Navigation Guidance Law Proportional Navigation Law Roll-pitch seeker Missile Acceleration Proportional Navigation seeker Seeker Stabilization Loop Sideslip Angle Stabilized platform based seeker