《飛彈制導原理》是2012年出版的圖書，作者是江加和。
基本介紹
- 中文名：飛彈制導原理
- 作者：江加和
- 出版時間：2012年6月
- 頁數：312 頁
- 定價：69 元
- ISBN：9787512407527
- 出版社：北京航空航天大學出版社
- 副標題：飛彈制導原理
內容介紹
《飛彈制導原理》內容：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,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 personnel engaged in the design anddevelopment of guided missiles.
