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拦截高速机动目标三维联合比例制导律设计

李辕 赵继广 闫梁 白国玉

李辕, 赵继广, 闫梁, 等 . 拦截高速机动目标三维联合比例制导律设计[J]. 北京航空航天大学学报, 2015, 41(5): 825-834. doi: 10.13700/j.bh.1001-5965.2014.0335
引用本文: 李辕, 赵继广, 闫梁, 等 . 拦截高速机动目标三维联合比例制导律设计[J]. 北京航空航天大学学报, 2015, 41(5): 825-834. doi: 10.13700/j.bh.1001-5965.2014.0335
LI Yuan, ZHAO Jiguang, YAN Liang, et al. United-proportional-navigation law for interception of high-speed maneuvering targets[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(5): 825-834. doi: 10.13700/j.bh.1001-5965.2014.0335(in Chinese)
Citation: LI Yuan, ZHAO Jiguang, YAN Liang, et al. United-proportional-navigation law for interception of high-speed maneuvering targets[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(5): 825-834. doi: 10.13700/j.bh.1001-5965.2014.0335(in Chinese)

拦截高速机动目标三维联合比例制导律设计

doi: 10.13700/j.bh.1001-5965.2014.0335
基金项目: 国家“863”计划
详细信息
    作者简介:

    李辕(1986—),男,山西阳泉人,博士研究生,bartholomew_lee@hotmail.com

    通讯作者:

    赵继广(1967—),男,山东日照人,教授,zjgbeijing@126.com,主要研究方向为航天任务分析与设计.

  • 中图分类号: V412.1

United-proportional-navigation law for interception of high-speed maneuvering targets

  • 摘要: 针对高速机动目标,提出了三维联合比例制导律.该制导律通过时变导航比将顺、逆轨拦截优势相结合,由2个平面制导律合成三维制导律后,可实现顺顺轨、逆逆轨和顺逆轨结合3种拦截模式,极大地扩展了经典比例制导律捕获区域.在二维条件下,根据目标加速度推导了视线角速率的解析式,设计了时变导航比.将二维联合比例制导律扩展到三维,修正了之前算法中俯仰平面的拦截弹路径倾角与速度计算误差,并给出了目标加速度背离拦截弹的机动模型.仿真结果表明:对于高速机动目标,联合比例制导律捕获区域更大,且较经典比例制导律和负比例制导律脱靶量更低、较增广比例制导律控制力更小.

     

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出版历程
  • 收稿日期:  2014-06-09
  • 修回日期:  2014-07-02
  • 刊出日期:  2015-05-20

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