摘要
为得到脉冲控制激光半主动末段修正弹落点精度更高的修正力作用方向,提出在传统点火相位计算基础上加入落点预测补偿,并通过建立激光探测器目标方位模型,结合脉冲力的纵向和横向修正能力的分析,推导出改进后的点火相位。采用六自由度弹道仿真进行验证,结果表明,采用文中点火相位进行弹道修正后,落点偏差明显减小,平均脱靶量从56.3m减小到13.1m,圆概率误差从48.1m减小到12.4m,证明了该方法的有效性,为末段修正弹控制策略的设计提供了理论依据。
To get the direction of correction force which leads to the higher impact-point accuracy of semi-active laser impulse terminal correction projectile(TCP),a new method of impact point prediction compensation added to the calculation of traditional firing phase angle was proposed. The target-orientation model of laser detector was established.The improved firing phase angle was deduced by analyzing the longitudinal and lateral correction capability by impulse forces.A 6-DOF trajectory simulation was used to validate the proposed method.The results show that the average miss distance decreases from 19.9 m to 13.1 m,and the circular error probability decreases from 27.7m to 12.4m after the ballistic correction under the proposed firing phase angle compared with the traditional firing phase angle.The proposed method is effective,and it provides a theoretical basis for the design of control strategy of TCP.
出处
《弹道学报》
CSCD
北大核心
2014年第4期66-71,共6页
Journal of Ballistics
基金
中央高校基本科研业务费专项资金资助(30920130122001)
关键词
末修弹
落点预测
末段修正
激光半主动
脉冲修正
点火相位
terminal correction proj ectile
impact point prediction
terminal correction
semi-active laser
impulse correction
firing phase angle