节点文献
火箭被动控制技术机理研究
A STUDY ON MECHANISM OF VOCKET PESSIVE CONTVOLLER
【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.其后的火箭弹缺陷不产生弹道偏差
【Abstract】 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.
- 【文献出处】 弹道学报 ,Journal of Ballistics , 编辑部邮箱 ,1991年03期
- 【被引频次】5
- 【下载频次】64