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基于速度预测的导引律剩余时间估计

张友安 梁勇 刘京茂 孙玉梅

张友安, 梁勇, 刘京茂, 等 . 基于速度预测的导引律剩余时间估计[J]. 北京航空航天大学学报, 2017, 43(10): 1980-1986. doi: 10.13700/j.bh.1001-5965.2016.0782
引用本文: 张友安, 梁勇, 刘京茂, 等 . 基于速度预测的导引律剩余时间估计[J]. 北京航空航天大学学报, 2017, 43(10): 1980-1986. doi: 10.13700/j.bh.1001-5965.2016.0782
ZHANG Youan, LIANG Yong, LIU Jingmao, et al. Time-to-go estimation for guidance laws based on velocity prediction[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(10): 1980-1986. doi: 10.13700/j.bh.1001-5965.2016.0782(in Chinese)
Citation: ZHANG Youan, LIANG Yong, LIU Jingmao, et al. Time-to-go estimation for guidance laws based on velocity prediction[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(10): 1980-1986. doi: 10.13700/j.bh.1001-5965.2016.0782(in Chinese)

基于速度预测的导引律剩余时间估计

doi: 10.13700/j.bh.1001-5965.2016.0782
基金项目: 

国家自然科学基金 61273058

中国博士后科学基金 20100471796

详细信息
    作者简介:

    张友安, 男, 博士, 教授。主要研究方向:先进控制理论与应用, 飞行器导航、制导与控制; 梁勇, 男, 博士, 副教授。主要研究方向:先进滤波理论与应用, 飞行器导航、制导与控制

    梁勇男,博士,副教授。主要研究方向:先进滤波理论与应用,飞行器导航、制导与控制

    通讯作者:

    梁勇, E-mail: ytliangyong@sina.com

  • 中图分类号: V448.13;TJ765

Time-to-go estimation for guidance laws based on velocity prediction

Funds: 

National Natural Science Foundation of China 61273058

China Postdoctoral Science Foundation 20100471796

More Information
  • 摘要:

    将分段线性逼近与迭代求解的思想扩展到对导弹的时变速度进行分段预测,给出了适用于反舰导弹速度时变情况的大前置角下比例导引律和偏置比例导引律的剩余时间估计算法。该算法在现有分段迭代算法的基础上,依据闭环形式的反舰导弹速度微分方程,分转弯平飞段和近似直线飞行段2种情况,对导弹未来速度的大小进行分段迭代预测并对剩余时间估计进行修正。算法中还给出了偏置比例导引律作用下近似直线飞行段剩余飞行航程的估计公式。仿真结果验证了本文算法的有效性。

     

  • 图 1  寻的制导示意图

    Figure 1.  Schematic diagram of homing guidance

    图 2  比例导引律情况仿真结果

    Figure 2.  Simulation results for proportional navigation guidance law

    图 3  偏置比例导引律情况仿真结果

    Figure 3.  Simulation results for biased proportional navigation guidance law

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出版历程
  • 收稿日期:  2016-10-10
  • 录用日期:  2016-12-23
  • 刊出日期:  2017-10-20

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