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以BLUE算法和GDOP为基本定位算法和精度分析工具,评估多基地雷达的定位性能,建立以GDOP最小值最小和有效监控区最大为目标的多基地雷达布站优化模型.仿真结果表明,通过以下措施可提高定位性能:①增加收发站总数;②采取扇形方式布站;③优先增加部署接收站;④交替部署收发站;⑤通过优化模型优化扇形布站分布角总和. 相似文献
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为了解决机动目标定位跟踪问题,提出了一种基于CS(current statistical)模型的交互式多模型粒子滤波算法.在交互式多模型粒子滤波算法的基础上,计算CS模型的概率,自适应地调整CS模型中的目标加速度,反映出了目标的机动特性,充分发挥2种算法的优点,改善了CS模型的加速度不能自适应调整的缺点,提高了CS模型的自适应性和应用范围.另外,CS模型的自适应滤波方法由Kalman滤波改为粒子滤波.通过Monte Carlo对比仿真试验表明了该算法的可行性和优越性. 相似文献
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针对色噪声环境下的MIMO雷达相干目标角度估计问题,提出一种基于目标信息矢量重构的角度估计算法.算法对MIMO雷达的接收数据进行了低复杂度改进,通过计算四阶累积量,得到一组矢量并证明该矢量包含所有目标的角度信息,通过重构Toeplitz矩阵,结合MUSIC算法实现了色噪声环境下MIMO雷达相干目标的角度估计.算法保留了MIMO雷达的阵元扩展能力和目标分辨力,具有自动抑制加性高斯白噪声和色噪声的能力,实现了相干目标的有效估计,更利于在实际中应用.最后计算机仿真结果证实了算法的有效性和可行性. 相似文献
237.
《防务技术》2022,18(9):1546-1551
In the present study, thermal hazards of TNT and DNAN used as the molten binder in TKX-50-based melt-cast explosives were comparatively studied through accelerating rate calorimeter (ARC) and Cook-off experiments. Two kinds of ARC operation modes were performed to investigate the thermal safety performance under adiabatic conditions (HWS mode) and constant heating (CHR mode). The obtained results demonstrated that at both heating modes, DNAN/TKX-50 outperformed TNT/TKX-50 from the thermal safety point of view. However, the sensitivity to heat of the samples was reverse because of the different heating modes. In addition, the results of thermal hazard assessment obtained from the cook-off experiment complied with ARC analysis which indicated the molten binder TNT replaced by DNAN would reduce the hazard of the TKX-50 melt cast explosive. Furthermore, the results of cook-off experiments also showed that DNAN/TKX-50 outperformed TNT/TKX-50 from the aspect of thermal stability, which was consistent with the result of CHR mode because of the similar heating process. 相似文献
238.
采用工作结构分解(Work Breakdown Structure,WBS)和风险结构分解法(Risk Breakdown Structure,RBS)对装备保障综合演练全过程的风险及其风险因素进行了系统分析,得出了装备保障综合演练过程中存在的7类风险、24种风险因素;运用网络层次分析法(Analytic Network Process,ANP)对各种风险及其风险因素进行了评估,得出了其对装备保障综合演练风险影响的权重及排序。研究结果可为装备保障综合演练顺利开展,确保人员、装备安全提供参考。 相似文献
239.
《防务技术》2014,10(2):101-105
Both heating and solvent-spray methods are used to consolidate the standard grains of double-base oblate sphere propellants plasticized with triethyleneglycol dinitrate (TEGDN) (TEGDN propellants) to high density propellants. The obtained consolidated propellants are deterred and coated with the slow burning multi-layer coating. The maximum compaction density of deterred and coated consolidated propellants can reach up to 1.39 g/cm3. Their mechanic, deconsolidation and combustion performances are tested by the materials test machine, interrupted burning set-up and closed vessel, respectively. The static compression strength of consolidated propellants deterred by multi-layer coating increases significantly to 18 MPa, indicating that they can be applied in most circumstances of charge service. And the samples are easy to deconsolidate in the interrupted burning test. Furthermore, the closed bomb burning curves of the samples indicate a two-stage combustion phenomenon under the condition of certain thickness of coated multi-layers. After the outer deterred multi-layer coating of consolidated samples is finished burning, the inner consolidated propellants continue to burn and breakup into aggregates and grains. The high burning progressivity can be carefully obtained by the smart control of deconsolidation process and duration of consolidated propellants. The preliminary results of consolidated propellants show that a rapid deconsolidation process at higher deconsolidation pressure is presented in the dynamic vivacity curves of closed bomb test. Higher density and higher macro progressivity of consolidated propellants can be obtained by the techniques in this paper. 相似文献
240.