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弹道学报  2015 

空空导弹动态攻击区的高精度快速算法研究

Keywords: 空空导弹,动态攻击区,平移数值算法,改进进退法

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Abstract:

针对空空导弹攻击区计算的快速性与高精确度之间的矛盾,以及考虑到在真实空战环境中机载计算机对动态攻击区实时在线计算的需要,在改进的进退法的基础上提出了平移数值算法。由改进的进退法计算出无风场干扰、目标不机动时的三维导弹攻击区,采用平移数值算法,计算实战环境中存在风场干扰和目标机动条件下的导弹动态攻击区。仿真结果表明,该平移数值算法具有实时在线与高精确度的特点,可以为实际空战中导弹动态攻击区的计算,以及载机上的空空弹发射系统设计等提供技术参考,并且可以推广到其它各种类型导弹的动态攻击区的实时在线和高精确度的数值计算。

References

[1]  易华,谢希权.基于自适应模糊系统的多目标导弹攻击区解算[J].系统工程与电子技术,2002,24(1):45-47.
[2]  YI Hua,XIE Xi-quan.Algorithm for the missile launching envelope in multi-target attacking based on the adaptive fuzzy system[J].Systems Engineering and Electronics,2002,24(1):45-47.(in Chinese)
[3]  刘代军,高晓光,李言俊,等.中远程空空导弹允许攻击区的快速模拟算法[J].西北工业大学学报,1999,17(4):530-533.
[4]  LIU Dai-jun,GAO Xiao-guang,LI Yan-jun,et al.A fast simulation algorithm for calculating the allowable attack area for air-to-air missiles[J].Journal of Northwestern Polytechnical University,1999,17(4):530-533.(in Chinese)
[5]  王宏伦,佟明安.空空导弹攻击区处理的拟合――插值法[J].火力与指挥控制,1998,23(4):14-18.
[6]  WANG Hong-lun,TONG Ming-an.A hybrid method of least square fit and interpolation used in the approximation of air-to-air missile launch envelopes[J].Fire Control & Command Control,1998,23(4):14-18.(in Chinese)
[7]  张列航,雷蕾,杨长启.中程空空导弹攻击区仿真与拟合[J].航空科学技术,2010(4):25-27.
[8]  ZHANG Lie-hang,LEI Lei,YANG Chang-qi.Attack area calculating and data fitting for medium air-to-air missile[J].Aeronautical Science & Technology,2010(4):25-27.(in Chinese)
[9]  雷科,林忠贤.制导炸弹攻击区拟合算法研究[J].电光与控制,2013,20(2):85-88.
[10]  LEI Ke,LIN Zhong-xian.A fitting algorithm for calculating attack envelope of guided bombs[J].Electronics Optics & Control,2013,20(2):85-88.(in Chinese)
[11]  黄国强,南英,陈芳.基于BP神经网络的有控炸弹攻击区拟合分析[J].弹箭与制导学报,2009,29(3):217-220.
[12]  HUANG Guo-qiang,NAN Ying,CHEN Fang.Attack zone fitting and Matlab simulation of guided-bomb based on BP neural network[J].Journal of Projectiles,Rockets,Missiles and Guidance,2009,29(3):217-220.(in Chinese)
[13]  黄国强,南英,陈芳,等.考虑各种随机干扰源有控炸弹攻击区及弹道仿真研究[J].弹箭与制导学报,2009,29(5):193-196.
[14]  HUANG Guo-qiang,NAN Ying,CHEN Fang,et al.Attack zone and trajectory simulation of guided-bomb considering many kinds of stochastic interference source[J].Journal of Projectiles,Rockets,Missiles and Guidance,2009,29(5):193-196.(in Chinese)
[15]  吴胜亮,南英,黄国强,等.随机风场与升阻比误差对空空导弹攻击区的敏感度研究[J].弹道学报,2012,24(2):25-30.
[16]  WU Sheng-liang,NAN Ying,HUANG Guo-qiang,et al.Attack zone sensitivity of air-to-air missile caused by random wind and error of lift-drag ratio[J].Journal of Ballistics,2012,24(2):25-30.(in Chinese)
[17]  黄国强,南英,陈芳.无动力滑翔弹最优抛射初始条件研究[J].飞行力学,2009,27(1):93-95.
[18]  HUANG Guo-qiang,NAN Ying,CHEN Fang.Optimal release conditions of no-power gliding bomb[J].Flight Dynamics,2009,27(1):93-95.(in Chinese)
[19]  钱杏芳,林瑞雄,赵亚男.导弹飞行力学[M].北京:北京理工大学出版社,2000.
[20]  QIAN Xing-fang,LIN Rui-xiong,ZHAO Ya-nan.Missile flight mechanics[M].Beijing:Beijing Institude of Technology Press,2000.(in Chinese)
[21]  LINDZEN R S.Turbulence and stress owing to gravity wave and tidal breakdown[J].Journal of Geophysical Research,1981,86(C10):9 707-9 714.
[22]  YU Yong-hui.A numerical model characterizing internal gravity wave propagation into the upper atmosphere[J].Advances in Space Research,2009,44(7):836-846.

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