北京航空航天大學「空間技術應用」系列叢書：導彈制導原理

　　The intent of this book is to present guidance and control principle of tactical missiles. It includes basicconcepts of guided missile， fundamental concepts of vehicle dynamics， dynamical equations and kinematicequations of vehicle， longitudinal state equation and transfer functions， lateral state equation and transferfunctions， fundamental principle of missile guidance and control system， guidance laws， autopilot design，comm. and guidance systems， homing guidance systems， and guidance and control system hardware-in-the-loopsimulation.
　　This book is suitable for international postgraduate and advanced undergraduates majoring in navigation，guidance and control， and also suitable for engineering and technical personnel engaged in the design and development of guided missiles.

CHAPTER 1 Introduction to Missile Guidance
1.1 Development History of Rockets and Missiles
1.2 Categories of Guided Missiles
1.3 Missile Guidance Systems
1.4 Introduction to Command Guidance System
1.5 Introduction to Homing Guidance System
1.5.1 Basic Concept and Classification of Homing Guidance System
1.5.2 Introduction to Seeker
1.6 Brief Introduction to Guidance Laws
1.7 Autopilots
1.8 Outline of the Book
References

CHAPTER 2 Basic Knowledge of Flight Dynamics
2.1 Coordinate Frames
2.2 Motion Parameters
2.3 Geometrical Parameters of Vehicle
2.4 Forces and Moments Acting on Vehicle
2.4.1 Gravity
2.4.2 Thrust
2.4.3 Aerodynamic Forces
2.4.4 Aerodynamic Moments
2.5 Hinge Moments of Control Surfaces
References

CHAPTER 3 Equations of Motion for Vehicle
3.1 Introduction
3.2 Dynamic Equations
3.2.1 Force Equations
3.2.2 Moment Equations
3.3 Kinematical Equations
3.3.1 Kinematical Equations of the Mass Center of Vehicle
3.3.2 Angular Motion Equations
3.4 Small-disturbance Theory
References

CHAPTER 4 Longitudinal Motion
4.1 State Variable Representation of the Linearized Longitudinal Equations
4.2 Longitudinal Transfer Functions
4.3 Longitudinal Approximations
4.3.1 Short-period Approximation
4.3.2 Short-period Approximation Transfer Function
4.3.3 Effect of Altitude and Airspeed on Short-period Mode Characteristic
Parameters
4.3.4 Long-period Motion Approximation
4.3.5 Effect of Altit.ude and Airspeed on Long-period Mode Characteristic
Parameters
4.4 Effects of the Variation of Aerodynamic Derivatives on the Longitudinal
Motion
4.5 Solution of the Longitudinal Equations （Control Surface Locked）
4.6 Transient Response of Vehicle
4.7 AnIntegrated Example
References

CHAPTER 5 Lateral Motion
5.1 State Variable Representation of the Linearized Lateral Equations
5.2 LateraI Transfer Functions
5.3 LateraI Approximations
5.3.1 RoII Approximation
5.3.2 Effect of Altitude and Airspeed on Roll Mode Characteristic Parameters
……
CHAPTER 6 Flight Control of Missile
CHAPTER 7 Guidance Laws
CHAPTER 8 Autopilot Design
CHAPTER 9 Command Guidance Systems
CHAPTER 10 Homing Guidance Systems
CHAPTER 11 Hardware-in-the-Ioop Simulation of Guidance and Control System