弹道学报2011，Vol.23Issue(2)：57-61,5.
基于粒子群算法的防空修正弹控制方法研究
Research on Control Method of Anti-aircraft Correction Ammunition Based on Particle Swarm Optimization
摘要
Abstract
In order to improve the ability of anti-aircraft trajectory correction ammunition to intercept maneuvering targets, a control method of missile-borne actuator was proposed. The particle trajectory model was established. According to the basic principle of trajectory correction, the optimal model of impulsive control was obtained. The ignition pulse control strategy was given according to the characteristics of impulse control. The particle swarm optimization (PSO) was applied to optimizing the impulsive control instructions. By introducing the minimum consumption principle of pulse energy, the fitness function was improved. The overall optimal solutions of control instructions were searched. Simulation results show that this control method can make anti-aircraft ammunition gain high hit-precision to intercept maneuvering target.关键词
弹道/粒子群算法/防空弹道修正弹/脉冲控制Key words
trajectory/particle swarm optimization/anti-aircraft trajectory correction ammunition/impulsive control分类
军事科技引用本文复制引用
杨红伟,甘明刚..基于粒子群算法的防空修正弹控制方法研究[J].弹道学报,2011,23(2):57-61,5.基金项目
北京市教育委员会共建基金项目(XK100070532) （XK100070532）
省部级重点基金项目(9140A17051010BQ0104) （9140A17051010BQ0104）
