a thorough overview of missile autopilot

[书籍]导弹制导与控制原理 很不错的书 推荐给大家-Missile guidance and control theory

针对某些导弹在对目标进行打击时需要满足零脱靶量和攻击角度约束的要求,首先基于终端滑模控制和有限时间控制理论,改进了一种快速收敛的非奇异终端滑模函数,用于设计滑模面,结合自适应指数趋近律,提出了一种自适应非奇异终端滑模控制方法。(For some missile needs to meet the zero miss distance and attack angle constraint requirements in the attack on the target, based on the

A pressure vessel is designed to simulate stresses on missile components