摘要
本文提出了一种基于固体火箭发动机性能散布分析的固体导弹最大射程评定方法,将系统辨识、性能散布分析和统计分析有机结合,实用性强,对固体导弹试验鉴定技术研究具有重要意义。
in this paper, the maximum range evaluation method for solid missiles based on solid rocket motor performance dispersion analysis is presented. The method is the combination of system identification, performance dispersion analysis for solid rocket motor and range statistic analysis, which is practical and significant for solid missiles flight test qualification.
出处
《国防科技大学学报》
EI
CAS
CSCD
1999年第1期13-16,共4页
Journal of National University of Defense Technology