摘要
该文建立了求解折叠翼火箭满足散布极小化和飞行稳定性要求的最佳尾翼延时张开时问的数学模型和计算方法.实际算例说明了本方法的具体应用,且得到了与文献[1]形状相同的曲线.
The mathematical moled and computing method has been established in thispaper to find the optimal unfolding time of the wings of folded rockets on the request ofminimum dispersion and flying stability.Application of the method has been describedthrough practical sample,and the configuration of angular dispersion curve is the sameas one in Ref.[1].
出处
《弹道学报》
EI
CSCD
1993年第3期47-52,共6页
Journal of Ballistics
关键词
火箭
弹道
散布
rocket
ballistics
dispersion