Tactical Missile Design, Second Edition “扫描版，只能找到扫描版的，还可以” This is the first textbook offered for tactical missile design in over forty years. It is oriented toward the needs of aerospace engineering students, missile engineers, and missile program managers. It is intended to provide a basis for including tactical missile design as part of the aerospace engineering curriculum, providing new graduates with the knowledge they will need in their careers. The author’s decades of experience in the development of tactical missiles and their technologies is presented in an integrated handbook method for missile design. It uses simple closed-form analytical expressions that are physics-based to provide insight into the primary driving parameters. The text also provides example calculations of rocket-powered and ramjet-powered baseline missiles, typical values of missile parameters, examples of the characteristics of current operational missiles, discussion of the enabling subsystems and technologies of tactical missiles, and the current/projected state of the art of tactical missiles. Included with the text is a CD-ROM containing electronic versions of the figures; 29 videos showing examples of design considerations, development testing, manufacturing, and technologies; 6 design case studies; configuration sizing methods; and an aerospace engineering outreach program for middle school students.

计算导弹的气动参数，可以不用进行cfd计算就得到大致气动数据

MISSILE DATCOM，经典的气动计算软件。

Airborne Vehicle Guidance and Control Systems is a broad and wide- angled engineering and technological area for research, and continues to be important not only in military defense systems but also in industrial process control and in commercial transportation networks such as various Global Positioning Systems (GPS). The book fills a long-standing gap in the literature. The author is retired from the Air Force Institute and received the Air Force's Outstanding Civilian Career Service Award.

已上传GitHub，已关闭动态调分 本文基于MATLAB Simulink Missile Guidance模型，目的在于： 1、了解导航制导与控制的基本概念，以及GNC系统的作用和组成部分； 2、以导弹飞行力学为基础，完成GNC系统的建模； 3、了解半实物仿真的意义，工作原理，以及半实物仿真实验的实施过程； 4、学习使用MATLAB/Simulink软件搭建导弹弹体及制导控制回路模型，通过实验加深对课堂所学相关知识的理解； 5、设计一个制导系统，完成数字仿真实验。

本文基于MATLAB Simulink Missile Guidance模型，目的在于： 1、了解导航制导与控制的基本概念，以及GNC系统的作用和组成部分； 2、以导弹飞行力学为基础，完成GNC系统的建模； 3、了解半实物仿真的意义，工作原理，以及半实物仿真实验的实施过程； 4、学习使用MATLAB/Simulink软件搭建导弹弹体及制导控制回路模型，通过实验加深对课堂所学相关知识的理解； 5、设计一个制导系统，完成数字仿真实验。

USAF Missile DATCOM source code to extract aerodynamic parameters of missile very powerful tool for engineers and designers

比例导航制导律发出加速度指令，垂直于导弹目标的瞬时视线，与视线速率和接近速度成正比

Missile datcom与matlab匹配程序，为初学者提供资源。为贡献作者工作，收取一积分

战术导弹设计PPT，很好的教材，值得一看。有需要的请下载