作者：江加和
页数：312
出版社：北京航空航天大学出版社
出版日期：2012
ISBN：9787512407527
电子书格式：PDF
PDF下载地址
内容简介
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 equatio and kinematicequatio of vehicle,
longitudinal state equation and trafer functio, lateral state
equation and traferfunctio, fundamental principle of missile
guidance and control system, guidance laws, autopilot
design,command 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 peonnel engaged in the
design anddevelopment of guided missiles.
本书特色
this book consists of elevenchapters.
chapter 1 introduces basic concepts of guided missile. chapter 2
presents thefundamental concepts of vehicle dynamics. the forces
and moments acting on the vehicle arealso presented. chapter 3
discusses vehicle dynamical equations and kinematic equations.based
on small-disturbance theory, chapter 4 discusses vehicle
longitudinal state equationsand transfer functions. chapter 5 deals
with lateral state equations and transfer functions.chapter 6
presents fundamental principle of missile guidance and control
system. chapter 7focuses on guidance laws. autopilot design is
discussed in chapter 8. chapter 9 is devoted tocommand guidance
systems. chapter 10 focuses on homing guidance system. chapter 11
summarizes guidance and control system hardware-in-the-loop
simulation.
目录
chapter 1 introduction to missile guidance
chapter 2 basic knowledge of flight dynamics
chapter 3 equatio of motion for vehicle
chapter 4 longitudinal motion
chapter 5 lateral motion
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-loop simulation of guidance and control
system