摘要
本文论述了火箭被动控制器的力学模型,并给出了计算机模拟其发射过程的结果.结果分析表明:火箭弹缺陷的初始方位的随机性不影响被动控制效果.火箭弹的弹道偏差产生于发动机点火后的很短时间之内.
physics model of rocket passive controller is discussed in the report. the computer simulation re-sults of the launching procsess are given. They show that randomness of the initial direction of rocket's er-rors do not affect the property of passive controller, and that ballistics errors are produced in shot time af-ter firing, after that, the ro-cket's errors wiu not make bauistics error in-creasing.
出处
《弹道学报》
EI
CSCD
1991年第3期61-64,共4页
Journal of Ballistics
关键词
火箭
发射
被动控制
rocket
launching
passive control
