弹道学报2011，Vol.23Issue(4)：1-4,4.
远程火箭末敏弹弹道特性仿真
Simulation of Ballistic Characteristics of Long-Range-Rocket Target-Sensitivity-Projectile
摘要
Abstract
To study the ballistic characteristics of long-range-rocket target-sensitivity-projectile,the ballistic equations of long-range-rocket target-sensitivity-projectile were established.Considering the jointing mode and binding,the dynamic relations of rigid bodies among parachute,plate and projectile were studied.The elasticity of the parachute rope was analyzed.The integrated motion model in decelerating and stable scanning period was established.The simulation software for long-range-rocket target-sensitivity-projectile was compiled,and the numerical simulation was carried out.The simulation results were validated by some experiment results.The ballistic characteristics of target-sensitivity-projectile were analyzed.The study lays foundation for simulation of firing precision and decreasing rockets consuming in test of long-range-rocket target-sensitivity-projectile.关键词
远程火箭/末敏弹/弹道特性/仿真Key words
long-range-rocket/target-sensitivity-projectile/ballistic characteristic/simulation分类
军事科技引用本文复制引用
王国平,芮筱亭,张驰,辛松..远程火箭末敏弹弹道特性仿真[J].弹道学报,2011,23(4):1-4,4.基金项目
国家自然科学基金项目 （）
新世纪优秀人才支持计划基金项目 （）
南京理工大学自主科研专项计划基金项目 （）
