Tactical missile guidance and control system design

1 The Overview of Missile Guidance and Control
2 Missile Mathematical Models
2.1 Symbols and Definitions
2.2 Euler Equations of the Rigid Body Motion
2.3 Configuration of the Control Surfaces
2.4 Missile Aerodynamic Derivatives and Dynamic Coefficients
2.5 Aerodynamic Transfer Functions of the Missile
3 Simplified Models of Missile Control Components
4 Guidance Radar
4.1 Introduction
4.2 Motion Characteristic of Line of sight
4.3 Control Loop of the Guidance Radar
4.4 Effect of the Receiver Thermal Noise on the Guidance Performance
4.5 Effect of Target Glint on the Guidance Performance
4.6 Effect of Other Disturbances on the Guidance Performance
5 Seekers
5.1 Definitions
5.2 Different Kinds of Seekers
5.3 Antidisturbance Moment of the Seeker
5.4 Body Motion Coupling and the Parasitic Loop
5.5 A Real Seeker Model
5.6 Other Parasitic Loop Models
5.7 Platform Based Seeker Design
6 Missile Autopilot Design
6.1 Acceleration Autopilot
6.2 Pitch/Yaw Attitude Autopilot
6.3 Flight Path Angle Autopilot
6.4 Roll Attitude Autopilot
6.5 BTT Missile Autopilot
6.6 Thrust Vector Control and Thruster Control
6.7 Spinning Missile Control
7 Line of Sight Guidance Methods
7.1 LOS Guidance System
7.2 Required Acceleration for the Missile with LOS Guidance
7.3 Analysis of the LOS Guidance Loop
7.4 Lead Angle Guidance Method
8 Proportional Navigation and Extended Proportional Navigation Guidance Laws
8.1 Proportional Navigation Guidance Law
8.2 Optimal Proportional Navigation Guidance Laws （OPN）
8.3 Other Proportional Navigation Laws
8.4 Target Acceleration Estimation
8.5 Optimum Trajectory Control System Design
9 Optimal Guidance for Trajectory Shaping
9.1 Optimality of Error Dynamics in Missile Guidance
9.2 Optimal Predictor corrector Guidance
9.3 Gravity turn assisted Optimal Guidance Law
9.4 Three dimensional Optimal Impact Time Guidance for Antiship Missiles
References