电光与控制, 2014, 21 (9): 95, 网络出版: 2014-09-15
中距拦射空空导弹的中制导指令计算新方法
MidGuidance Instruction Calculation of Medium Range Air to Air Intercept Missile
中距拦射导弹 中制导指令 变周期 当前统计模型 mediumrange intercept missile midguidance instruction variable period current statistical model
摘要
介绍了经典中距拦射空空导弹无线电修正指令的形成原理及存在的问题,并分析了原因。提出了变周期中制导指令的方式,并建立了基于目标当前统计模型的变周期指令模型,将目标运动状态预估计值融入中制导指令,以中制导剩余时间估计为根据,改变中制导指令周期。仿真结果表明,改进的指令模型提高了导引头偏离角跟踪的效能并限制了截获时的目标指示角误差。
Abstract
The principle and the existing problems of radio amendment instruction consisted in the classical mediumrange airtoair intercept missile are described. Then a new method of variable period midguidance instruction is proposed. A variable period instruction model is established based on the Current Statistical Model (CSM) of target. The predicted target motion value is introduced into midguidance instruction,and the period of midguidance instruction is changed according to the estimated remaining time of midguidance. The simulation result indicates that the modified instruction model can improve the tracking efficiency of seeker and limit the error of targets designation angle in intercepting and capturing.
康志强, 寇英信, 李战武, 陈磊. 中距拦射空空导弹的中制导指令计算新方法[J]. 电光与控制, 2014, 21(9): 95. KANG Zhiqiang, KOU Yingxin, LI Zhanwu, CHEN Lei. MidGuidance Instruction Calculation of Medium Range Air to Air Intercept Missile[J]. Electronics Optics & Control, 2014, 21(9): 95.