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missile
- 空地导弹全弹道仿真建模(说明文件)：自由下滑段+固定倾角下滑+转平飞过渡段+平飞段+导引段-missile simulation/matlab
best1
- a thorough overview of missile autopilot
Missile-guidance-and-control-theory
- [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
ml-driver_mldriver.c.pdf
- Dream Cheeky USB Missile Launcher driver module
ml-driver_mlmanage.sh.pdf
- Dream Cheeky USB Missile Launcher driver shell scr ipt
ml-driver_user-space.c.pdf
- Dream Cheeky USB Missile Launcher driver client
6
- the pdf file of AIAA journal paper which was downloaded from its site and it is about MD(missile datcom)
PDF+simulink
- 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
10.2514@6.1981-589.pdf
- To ensure the launch tube design according with the theoretical design requirements, the stress and displacement of the launch tube under the maximum load were analyzed in comparison. The results reflected that the stiffness and intensity of launch t
1-s2.0-S1877705813016950-main.pdf
- A pressure vessel is designed to simulate stresses on missile components