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Analysis of Design Parameters Based on Bullet Trajectories and Hit Probability

机译:基于子弹轨迹和命中概率的设计参数分析

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The parameters related to hit probability for optimal design of combat vehicles affects the performance of fire power. In this paper, we present the procedure how to obtain maximal allowable ranges of design parameters so that the desired hit probability may be achieved. To satisfy the desired hit probability, the design parameters should be confined in some regions. For simulation, assume that two design parameters, muzzle velocity error and gun pitch angle error, play major roles for hit probability prediction. The variation of design parameters results in dispersion of bullets at the target plane. Measuring dispersion at the target is called as an error estimate. We use the experimental approach as the error estimate. Experimental approach uses the unit partial and estimation of total errors. Total errors of muzzle velocity and gun pitch angle are transferred to the total errors at the target through the trajectory equation. The unit partials mean the ratio of the error at the target to that at the fire position. In this paper we use both exact trajectory and approximate trajectory. We are able to obtain the maximal allowable range of errors of both muzzle velocity and gun pitch angle in order to achieve the desired hit probability. To satisfy a given hit probability for the given range, it is shown that the vertical gun pitch angle error and muzzle velocity error should be confined into a first quadrant of an elliptic region.
机译:与战斗机最佳设计的命中概率有关的参数影响着火力的性能。在本文中,我们介绍了如何获得设计参数的最大允许范围的过程,以便可以实现所需的命中概率。为了满足期望的命中概率,应将设计参数限制在某些区域。为了进行仿真,假设枪口速度误差和枪身俯仰角误差这两个设计参数在命中概率预测中起主要作用。设计参数的变化导致子弹在目标平面上的分散。在目标处测量色散称为误差估计。我们使用实验方法作为误差估计。实验方法使用部分误差和总误差的估计。炮口速度和炮距角的总误差通过轨迹方程传递到目标处的总误差。单位局部误差是指目标位置与射击位置处的误差之比。在本文中,我们同时使用精确轨迹和近似轨迹。我们能够获得枪口速度和炮距角的最大误差范围,以实现所需的命中概率。为了在给定的范围内满足给定的命中概率,表明垂直枪的俯仰角误差和枪口速度误差应被限制在椭圆形区域的第一象限内。

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