搜索资源列表
coe_gui
- 空空导弹设计,可以全面的介绍,分析空空导弹的一般控制和分析流程-Air-to-air missile designed to introduce a comprehensive analysis of air-to-air missile control and analysis of the general process
missle--control--design
- 导弹控制系统鲁棒设计程序源代码,可以用来参考编程,比较实用-missile control system design
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
MissileSim
- 导弹飞行控制 3自由度动力学仿真 质点运动学仿真(Missile flight control)
复合控制模式制导(滑模加直接力)
- 复合控制模式下的导弹拦截仿真,运用滑模控制方法与直接力相结合的方式(The simulation of missile interception in compound control mode is based on the combination of sliding mode control and direct force)