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弹目信息在纯方位末制导中的应用
引用本文:魏玉乐,方群,罗建军.弹目信息在纯方位末制导中的应用[J].西北工业大学学报,2005,23(5):676-680.
作者姓名:魏玉乐  方群  罗建军
作者单位:西北工业大学,航天学院,陕西,西安,710072
摘    要:在考虑“被动测量”的条件下,探讨了通过综合利用弹目信息来获取制导所需信息的方法,设计了一种适合被动雷达寻的末制导的运动跟踪滑模制导律;根据自适应推广Kalman滤波技术设计了目标跟踪滤波器;给出了简化的末制导数学模型,并进行了仿真计算。结果表明:所给方法可以较好地提高导弹的制导精度。

关 键 词:弹目信息  纯方位末制导  运动跟踪滑模制导律  自适应推广Kalman滤波
文章编号:1000-2758(2005)05-0676-05
收稿时间:2004-12-02
修稿时间:2004年12月2日

Improving Bearings-Only Terminal Guidance through Estimating Position, Velocity, and Acceleration of Target Relative to Missile
Wei Yule,Fang Qun,Luo Jianjun.Improving Bearings-Only Terminal Guidance through Estimating Position, Velocity, and Acceleration of Target Relative to Missile[J].Journal of Northwestern Polytechnical University,2005,23(5):676-680.
Authors:Wei Yule  Fang Qun  Luo Jianjun
Abstract:In our opinion,the terminal guidance law can be improved by estimating missile-target parameters(relative position,velocity and acceleration) from bearings-only measurement in passive guidance mode.In the full paper,we explain in much detail how to make such an estimation;here,we give only a briefing.A Motion Tracking Sliding-Mode Guidance(MTSMG) law is proposed to enhance guidance accuracy for the nonlinear control systems of homing missile terminal guidance.We utilize the target-tracking AEKF(Adaptive Extended Kalman Filtering) algorithm to provide the above mentioned estimated information to MTSMG algorithm proposed by us.Based on simulations,the conclusions are as follows:(1) high guidance accuracy is obtained with MTSMG algorithm;(2) the terminal trajectory of homing missile is smooth;(3) the overload of missile is permissible and changes placidly.
Keywords:missile-target information  bearings-only terminal guidance  Motion Tracking Sliding-Mode Guidance(MTSMG)  Adaptive Extended Kalman Filtering(AEKF)
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