空天防御2024，Vol.7Issue(3)：64-71,8.
防空导弹双脉冲固体火箭发动机能量优化研究
Energy Optimization Research on Double-Pulse Solid Rocket Motor in Antiaircraft Missile
陈柯宇 1贾世伟 1顾嘉耀 1郑天宇 1陈好1
作者信息
摘要
Abstract
To resolve the problem of low terminal velocity of high and long-range ballistic missiles,combiningthe application of a double-pulse solid rocket motor in air defense missiles,this study analyzed the influence of thrust of the solid rocket motor and ignition interval of the two-stage engine on the terminal velocity of a high and long-range ballistic missile.Focusing on maximizing the terminal velocity of air defense missiles on highand long-rangetrajectories,the thrust and ignition interval of the double-pulse solid rocket motor were optimized using the improved Classified Chemical Reaction Optimization(CCRO)algorithms established in this study.Finally,the optimal energy distribution scheme for the motorenhancing the missile's terminal velocity was achieved.关键词
防空导弹/固体火箭发动机/能量优化/化学反应优化算法Key words
antiaircraft missile/solid rocket motor/energy optimization/chemical reaction optimization algorithms分类
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陈柯宇,贾世伟,顾嘉耀,郑天宇,陈好..防空导弹双脉冲固体火箭发动机能量优化研究[J].空天防御,2024,7(3):64-71,8.
