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 Antidisturbance 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 PitchYaw 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
內容試閱：
This book is pitched as an introductory text for tactical missiles，covering the missile systems and design processes that must be considered.The main contents of this book are the summary and extension of the authors 20 years research works in the field of missile guidance and control.
We start from Chapter 1 with the basics of missile guidance by exposing the reader to critical concepts such as lateral acceleration as the preferred guidance command，the interplay between guidance,navigation and control within the context of missile systems.Chapter 2 discusses the missile dynamics with detailed aerodynamic models.Chapter 3 is intended to present another brief overview of several pertinent missile subsystems and sensors，supposedly covering actuator dynamics，rate gyro dynamics，accelerometers and integrated navigation systems.Chapter 4 presents a discussion of the radar guidance system and attempts to extract this systems performance characteristics with the greatest impact on guidance loop design and overall system performance. Chapter 5 describes commonly used seekers and the parasitic loop and real seeker model.Details of how to design a proper missile autopilot are presented in Chapter 6，including the most wellknown twoloop and threeloop autopilot.Chapter 7 introduces the lineofsight guidance.The optimality of proportional navigation and its variants are discussed in Chapter 8.In the final chapter，we introduce some modern optimal guidance laws，including optimal trajectory shaping guidance and gravityturnassisted guidance.
The book can benefit researchers,engineers and graduate students in the field of Guidance，Navigation and Control.It is our hope for this book to serve as a useful step for permitting further advances in the field of missile guidance and control.The authors have carefully reviewed the content of this book before the printing stage.However，it does not mean that this book is completely free from any possible errors.Consequently，the authors would be grateful to readers who will call out attention on mistakes as they might discover.
Finally，the authors would like to thank colleagues from the Institute of Autonomous UAV Control，Beijing Institute of Technology for providing valuable and constructive comments.Without their support，the writing of the book would not have been a success.
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