摘要
建立了以弹性适配器作为被动控制器的火箭弹被动控制的数学模型，给出了数值模拟结果，并用以说明被动控制减小火箭推力偏心和动不平衡起的弹道散布的效果，最后阐明了火箭被动控制的机理。
A mathematical model of rocket passive control,in which elastic sabots are used as passive controllers is established.Some numerical results are presented.The results show the effectiveness of passive control in reducing the ballistic dispersion due to thrust misalignment and dynamic unbalance in the rocket.Finally,a description of the mechanism of rocket passive control is given.
出处
《兵工学报》
EI
CAS
CSCD
北大核心
1996年第1期40-45,共6页
Acta Armamentarii
关键词
被动控制
弹道散布
火箭弹
数学模型
rocket,elastic sabot,passive control,ballistic dispersion
