导弹制导原理
出版社：北京航空航天大学出版社
年代：2012
定价：55.0
书籍简介:
本书主要介绍战术导弹的制导控制原理。介绍弹内外制导控制设备，以及制导控制系统的分析与设计方法。全书共十一章。第一章介绍导弹的基本概念；第二章介绍飞行器动力学的基本概念；第三章介绍飞行器动力学方程和运动学方程；第四章介绍飞行器纵向状态方程和传递函数；第五章介绍飞行器侧向状态方程和传递函数；第六章介绍导弹制导控制系统的基本原理；第七章介绍制导律；第八章介绍自动驾驶仪；第九章介绍指令制导系统；第十章介绍寻的制导系统；第十一章介绍制导控制系统半实物仿真。
书籍目录:
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
内容摘要:
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.
编辑推荐:
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.
书籍规格:
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| 出版地 | 北京 | 出版单位 | 北京航空航天大学出版社 |
| 版次 | 1版 | 印次 | 1 |
| 定价(元) | 55.0 | 语种 | 英文 |
| 尺寸 | 26 × 19 | 装帧 | 平装 |
| 页数 | 印数 | ||
书籍信息归属:
导弹制导原理是北京航空航天大学出版社于2012.5出版的中图分类号为 TJ765.3 的主题关于 导弹制导－英文 的书籍。
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