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高动态条件下统计空时零陷加宽方法

张柏华 马红光 孙新利 谭巧英 潘寒尽

张柏华, 马红光, 孙新利, 谭巧英, 潘寒尽. 高动态条件下统计空时零陷加宽方法[J]. 电子与信息学报, 2016, 38(4): 913-918. doi: 10.11999/JEIT150654
引用本文: 张柏华, 马红光, 孙新利, 谭巧英, 潘寒尽. 高动态条件下统计空时零陷加宽方法[J]. 电子与信息学报, 2016, 38(4): 913-918. doi: 10.11999/JEIT150654
ZHANG Baihua, MA Hongguang, SUN Xinli, TAN Qiaoying, PAN Hanjin. Space Time Null Widening Method of Navigation Receiver in Missile for High Dynamic Conditions[J]. Journal of Electronics and Information Technology, 2016, 38(4): 913-918. doi: 10.11999/JEIT150654
Citation: ZHANG Baihua, MA Hongguang, SUN Xinli, TAN Qiaoying, PAN Hanjin. Space Time Null Widening Method of Navigation Receiver in Missile for High Dynamic Conditions[J]. Journal of Electronics and Information Technology, 2016, 38(4): 913-918. doi: 10.11999/JEIT150654

高动态条件下统计空时零陷加宽方法

doi: 10.11999/JEIT150654

Space Time Null Widening Method of Navigation Receiver in Missile for High Dynamic Conditions

  • 摘要: 论文根据弹载导航接收机的特点,建立了高动态环境的抗干扰模型;针对高动态环境下干扰的特点和传统零陷加宽方法的不足,提出新的基于统计的空时零陷加宽方法。该方法能在高动态条件和其它非理想因素引起的通道及数据失配的情况下有效地抑制干扰,大大增强弹载导航接收机抗干扰算法的鲁棒性。仿真试验表明了所提方法的有效性。
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    出版历程
    • 收稿日期:  2015-06-01
    • 修回日期:  2016-01-13
    • 刊出日期:  2016-04-19

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