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针对机载双基地雷达下视环境下非均匀地杂波的抑制问题,首先论述了抑制双基地机载雷达非均匀杂波的内插变换类空时自适应处理(space time adaptive processing,STAP)方法。然后在此基础上,提出了一种改进的空时二维内插变换方法(improved space time interpolation transfor-mation,ImSTINT)。该方法将训练样本的杂波子空间映射到单基地地基雷达的杂波子空间中,减少了变换后杂波子空间的自由度。仿真表明该方法比传统的内插变换类方法的杂波抑制性能好,且具有较强的稳健性和较少的样本量需求。 相似文献
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张媛 《中国人民武装警察部队学院学报》2011,27(5):82-85
深刻认识专门用途英语的特点以及专门用途英语在专业课教学中的重要作用,并根据专门用途英语教师的素质要求和武警学院专门用途英语教师队伍的现状,提出了专门用途英语教师队伍建设和提高专门用途英语教学质量的四种合作教学模式。 相似文献
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In order to predict the storage life of a certain type of HTPB (hydroyl-terminated polybutadiene) coating at 25 C and analyze the influence of pre-strain on the storage life, the accelerated aging tests of HTPB coating at 40 C, 50 C, 60 C, 70 C with the pre-strain of 0%, 3%, 6%, 9%, respectively were carried out. The variation regularity of the change of crosslinking density was analyzed and the aging model of HTPB coating under pre-strained thermally-accelerated aging was proposed. The storage life of HTPB coating at 25 C was estimated by using the Berthelot equation as the end point of the aging life with a 30% decrease in maximum elongation. The results showed that the change of crosslinking density of HTPB coating increased with the increase of aging temperature and aging time, and decreased with the in-crease of pre-strain. Under 0% pre-strain, the relationship between the change of crosslinking density of HTPB coating and the aging time can be described by the logarithmic model with the confidence probability greater than 99%.The stress relaxation phenomenon existed under 3%, 6% and 9% pre-strained aging. The aging model considering chemical aging and pre-strain was established with the confidence probability greater than 90%. The storage life of HTPB coating was 15.2935 years at 25 C under 0% pre-strain, which was reduced by 13.9007%, 75.6949% and 89.7859% under 3%, 6% and 9% pre-strain, respectively. The existence of pre-strain has a serious impact on the storage life of HTPB coating, therefore, the pre-strain should be avoided as much as possible during the actual storage. 相似文献
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针对当前雷达辐射源识别在低信噪比下识别率准确率不高,信号处理过程中难以很好保留有用信息的问题,提出了一种基于奇异谱修正香农熵(Singular Spectrum Modified Shannon Entropy,SSSE)的雷达调制信号识别方法.通过符号化聚合近似和奇异谱分析对雷达信号进行处理,求出信号的分类特征SSSE,通过分类器将处理后的信号进行分类.仿真结果显示,该方法在低信噪比范围下,仍有较高总体识别率,并且优于符号化聚合近似和奇异谱分析法. 相似文献
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Jian-hao Dou Xin Jia Zheng-xiang Huang Xiao-hui Gu Ying-min Zheng Bin Ma Qiang-qiang Xiao 《防务技术》2021,17(3):846-858
The use of a shaped liner driven by electromagnetic force is a new means of forming jets. To study the mechanism of jet formation driven by electromagnetic force, we considered the current skin effect and the characteristics of electromagnetic loading and established a coupling model of"Electric—Magnetic—Force"and the theoretical model of jet formation under electromagnetic force. The jet formation and penetration of conical and trumpet liners have been calculated. Then, a numerical simulation of liner collapse under electromagnetic force, jet generation, and the stretching motion were performed using an ANSYS multiphysics processor. The calculated jet velocity, jet shape, and depth of penetration were consistent with the experimental results, with a relative error of less than 10%. In addition, we calculated the jet formation of different curvature trumpet liners driven by the same loading condition and ob-tained the influence rule of the curvature of the liner on jet formation. Results show that the theoretical model and the ANSYS multiphysics numerical method can effectively calculate the jet formation of liners driven by electromagnetic force, and in a certain range, the greater the curvature of the liner is, the greater the jet velocity is. 相似文献
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Chain damage is a new phenomenon that occurs when a reactive jet impacts and penetrates multi-spaced plates.The reactive jet produces mechanical perforations on the spaced plates by its kinetic energy(KE),and then results in unusual chain rupturing effects and excessive structural damage on the spaced plates by its deflagration reaction.In the present study,the chain damage behavior is initially demonstrated by experiments.The reactive liners,composed of 26 wt%Al and 74 wt%PTFE,are fabricated through a pressing and sintering process.Three reactive liner thicknesses of 0.08 CD,0.10 CD and 0.12 CD(charge diameter)are chosen to carry out the chain damage experiments.The results show a chain rupturing phenomenon caused by reactive jet.The constant reaction delay time and the different penetration velocities of reactive jets from liners with different thicknesses result in the variation of the deflagration position,which consequently determines the number of ruptured plates behind the armor.Then,the finite-element code AUTODYN-3D has been used to simulate the kinetic energy only-induced rupturing effects on plates,based on the mechanism of behind armor debris(BAD).The significant discrepancies between simulations and experiments indicate that one enhanced damage mechanism,the behind armor blast(BAB),has acted on the ruptured plates.Finally,a theoretical model is used to consider the BAB-induced enhancement,and the analysis shows that the rupturing area on aluminum plates depends strongly upon the KE only-induced pre-perforations,the mass of reactive materials,and the thickness of plates. 相似文献