摘要
跟踪与分析国外先进防空导弹的姿控发动机控制技术,以美国PAC-3导弹为例,对姿控发动机组建立离散模型,然后采用一定的优化方法,对其点火方法作了研究,并提供仿真结果。
The side jet technology of foreign advanced surface-to-air missiles is analyzed, disperse thrust models of 180 attitude control engines of patriot-Ⅲ missile is built, and some optimized methods of ignite technology is studied, then the result of the simulation is presented.
出处
《现代防御技术》
北大核心
2007年第3期42-45,共4页
Modern Defence Technology
关键词
姿控发动机
点火逻辑
离散模型
仿真
attitude control engine
ignition logic
disperse model
simulation
