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近距引导战斗机自动攻击控制律实现
引用本文:陈中起,张斌,杜永伟,冯国强.近距引导战斗机自动攻击控制律实现[J].火力与指挥控制,2012,37(5):148-151,155.
作者姓名:陈中起  张斌  杜永伟  冯国强
作者单位:空军工程大学工程学院,西安,710038
摘    要:针对现代战斗机向目标空域的近距引导过程,建立了战斗机与目标相对运动的数学模型,提出了战斗机自动攻击的概念,并推导出一种基于瞄准误差的战斗机近距引导律。在此基础上,设计了近距引导战斗机自动攻击控制律。最后对基于瞄准误差的引导算法进行仿真,结果表明基于瞄准误差的近距引导方法很好地消除了瞄准误差,能够满足战斗机近距引导指标。

关 键 词:近距引导  瞄准误差  自动攻击  控制律

The Realization of Auto Attack Control Law for Short-distance Guidance of Fighter Plane
CHEN Zhong-qi , ZHANG Bin , DU Yong-wei , FENG Guo-qiang.The Realization of Auto Attack Control Law for Short-distance Guidance of Fighter Plane[J].Fire Control & Command Control,2012,37(5):148-151,155.
Authors:CHEN Zhong-qi  ZHANG Bin  DU Yong-wei  FENG Guo-qiang
Institution:(Engineering Institute,Air Force Engineering University,Xi’an 710038,China)
Abstract:In accordance with the short-distance guidance procedure for modern fighter plane to target airspace,firstly,the relative moving model of fighter plane and target is built,then,the auto-attack conception is put forward,and a kind of auto-attack guidance law of fighter plane based on sight error is given.Based on those,auto attack control law is designed.At last a simulation example is given whose results show that this method works perfectly to eliminate aiming error,and it is suitable for the auto-attack of aircraft.
Keywords:short-distance guidance  sight error  auto-attack  rule of control
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