滿額折
Guidance Principle of Missiles導彈制導原理（簡體書）
- ISBN13：9787512407527
- 出版社：北京航空航天大學出版社
- 作者：江加和
- 裝訂／頁數：平裝／312頁
- 規格：23.5cm*16.8cm (高/寬)
- 版次：1
- 出版日：2012/06/01
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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.
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.
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