排序方式: 共有114条查询结果,搜索用时 93 毫秒
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旋转弹体高速入水水中弹道的模拟方法 总被引:4,自引:1,他引:3
针对旋转弹体高速入水特点,从弹体运动的动力学方程和相似理论出发,提出了模拟旋转弹体高速入水水中弹道的马赫相似实验方案.该方案在大气环境条件下,能够实现原型和模型两系统的主要相似准数相等. 相似文献
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闭环校射中雷达跟踪弹迹的滤波和预测方法 总被引:2,自引:2,他引:0
闭环校射武器系统中,要求实时测量弹丸和目标之间的偏差,因此火控雷达要同时完成对弹丸运动和目标运动的跟踪任务,实现对弹丸目标的精确跟踪对火控雷达来说是一个新任务.建立了一种针对此类问题的滤波和预测方法,这种方法充分利用关于弹丸运动规律的已有知识,突破了常规动目标跟踪方法的限制,使滤波和预测误差比常规方法减小数倍,成功地解决了闭环校射武器系统中的一个技术难点. 相似文献
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某底排火箭复合增程弹为分体式结构,战斗部与发动机壳体通过螺纹联接,一次试验中弹丸在火炮约束期和半约束期内发生解体现象,弹体在与发动机壳体螺纹连接的根部发生断裂,通过对参试弹丸的相关参数和弹道跟踪雷达测得速度-时间曲线研究,以1943年空气阻力定律和炮兵用标准气象条件为研究方法,对解体前、后级弹丸的弹道参数和飞行阻力特性进行分析计算,还原了解体弹丸的实际弹道参数和飞行阻力特性,通过对分析结果与试验结果进行对比,分析结果与试验测得结果吻合较好,文中提到的研究方法可为弹丸弹道解体或零部件脱落的故障归零提供理论依据,在工程实际应用中有一定的参考价值。 相似文献
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高速旋转弹位置与姿态测量数据分析方法 总被引:1,自引:0,他引:1
精确的弹箭位置与姿态测量数据是提高制导弹箭射击精度的基础。通过分析高速旋转弹位置与姿态传感器的量测噪声,采用卡尔曼滤波方法进行误差估计,以提高测量精度。基于高速旋转弹质心运动和角运动方程,建立了系统状态方程;根据全球定位系统和地磁传感器的测量原理,建立了量测方程;以某弹飞行数据为例,采用扩展卡尔曼滤波(EKF)和无味卡尔曼滤波(UKF)分别对弹箭的位置和姿态进行最优估计。仿真结果表明,采用上述方法可有效减少系统误差,并使综合误差进一步降低,射程与高度误差均控制在±1 m,攻角和侧滑角误差分别为±0.02 rad和±0.01 rad,可满足工程应用的要求。 相似文献
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针对大口径火炮使用增程修正弹打远修近问题,建立了增程修正弹单炮多发同时弹着的控制算法,仿真验证了算法可在不同射程上实现单炮多发同时弹着,对发挥舰炮作战效能具有一定的意义。 相似文献
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速射转管炮作为近程反导武器系统的重要一员,射击精度影响着其最终防御效果,通过对速射转管炮特点及其射击偏差机理的分析,研究了转管炮射击过程中身管转速、弹丸初速等多种因素对射击精度的影响,并在转管炮初始设计、弹道模型和校射等方面提出了修正误差、提高射击精度的方法。 相似文献
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This study investigates and quantifies some possible sources affecting the position of impact points of small caliber spin-stabilized projectiles (such as 12.7 mm bullets). A comparative experiment utilizing the control variable method was designed to figure out the influence of tiny eccentric centroids on the projectiles. The study critically analyzes data obtained from characteristic parameter measurements and precision trials. It also combines Sobol's algorithm with an artificial intelligence algorithm—Adaptive Neuro-Fuzzy Inference Systems (ANFIS)—in order to conduct global sensitivity analysis and determine which parameters were most influential. The results indicate that the impact points of projectiles with an entry angle of 0° deflected to the left to that of projectiles with an entry angle of 90°. The difference of the mean coordinates of impact points was about 12.61 cm at a target range of 200 m. Variance analysis indicated that the entry angle — i.e. the initial position of mass eccentricity — had a notable influence. After global sensitivity analysis, the significance of the effect of mass eccentricity was confirmed again and the most influential factors were determined to be the axial moment and transverse moment of inertia (Izz Iyy), the mass of a projectile (m), the distance between nose and center of mass along the symmetry axis for a projectile (Lm), and the eccentric distance of the centroid (Lr). The results imply that the control scheme by means of modifying mass center (moving mass or mass eccentricity) is promising for designing small-caliber spin-stabilized projectiles. 相似文献
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《防务技术》2019,15(5):768-778
Annular grooved projectiles (AGPs) have drawn ongoing concerns as an advanced penetrator for their excellent anti-rebound capability in impacting metal plates. They could become embedded solidly in the target surface during low-velocity impact. In this investigation, the firm embedding behavior of AGP was observed by impact experiments. Corresponding numerical simulations provided a better understanding of this process. Experimental and numerical results indicated that the firm embedding behavior of AGP was mainly due to the filling-material in the groove rather than the friction between the projectile and target, unlike traditional shape such as conical projectile. According to observation, firm embedding process can generally be subdivided into four stages: initial-cratering stage, groove-filling stage, filling-material failure stage and rebound vibration stage. Moreover, the damage mechanics of target material around crater was obtained through microscopic tests. A comparison of the cross-sectional figures between the experiment and simulation proved that the analysis and the proposed method were reasonable and feasible, which further demonstrated that the firm embedding behavior has application potential in new concept warheads. 相似文献
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一维弹道修正弹是近年来兵器领域新研制的一种低成本信息化弹药,目前对其校射方法尚未有成熟的标准。为此,在分析一维弹道修正弹对岸射击工作原理、计算有无控弹试射的基础上,提出舰炮武器系统使用有控一维弹道修正弹的校射新方法,并确定了校射的组数和发数。分别对使用新方法前后的射击效能进行了数值仿真,结果表明本方法能极大地提高舰炮武器系统的射击效能。所提方法对舰炮武器作战效能的提高具有较强的理论价值和一定的参考意义。 相似文献