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Real-time Calculation for the Penetration Trajectory of Missile Based on Tri-axial Accelerometers

机译:基于三轴加速度计的导弹侵彻轨迹实时计算

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To solve the real time calculation problem that the trajectory of projectile will suffer from serious deflections when the missile penetrates into multilayer target plates consisting of vertical walls, we proposed a new method by applying two tri-axis accelerometers to acquire deflections of the projectile penetration angle and calculate the trajectory in the penetration. Based on the conventional formulas in the plane for calculating penetration depth for the penetration into the multilayer target, we concluded the real time calculation formulas for the trajectory of missile with two installed tri -axis accelerometers in the penetration, and performed finite element analysis for simulating the process of penetration using ABAQUS, and applied the acceleration data obtained from the simulation to calculate the penetration angle and traj ectory. Finally, applied algorithm developed in MATLAB to analyze the two group acceleration data of the two sets of accelerometers obtained from the simulation to verify the effectiveness of proposed algorithm.
机译:为解决导弹穿入由垂直壁组成的多层靶板时弹丸轨迹会严重偏斜的实时计算问题,提出了一种应用两个三轴加速度计获取弹丸穿透角偏斜的新方法。并计算出穿透的轨迹。基于平面上用于计算穿透多层目标的穿透深度的常规公式,我们得出了在穿透中安装两个三轴加速度计的导弹轨迹实时计算公式,并进行了有限元分析以进行仿真使用ABAQUS进行穿透过程,并应用从仿真中获得的加速度数据来计算穿透角和弹道。最后,应用MATLAB开发的算法对仿真得到的两组加速度计的两组加速度数据进行分析,验证了所提算法的有效性。

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