弹道中段碎片诱饵的数字仿真建模及分析OA
Digital simulation modeling and analysis of debris decoys in the ballistic midcourse
弹道导弹在中段飞行时产生的碎片群,对反导系统的目标识别构成重大挑战.为有效评估这些碎片诱饵的雷达散射特性,本文提出了一种"几何离散-动力学演化-电磁散射"一体化仿真方法.该方法首先将导弹壳体结构离散为三角面元;随后,结合改进的Gurney初速度模型与基于Rodrigues旋转变换的动力学迭代,模拟了爆炸后碎片群的时空演化过程.在此基础上,采用快速迭代的弹跳射线法对时变准静态的碎片群模型进行电磁散射计算.仿真分析了碎片云在不同擦地角下的雷达散射截面时变特性、一维距离像的能量扩散特征及角度散射特性.结果表明,所提模型能够有效模拟碎片的扩散过程极其复杂的,具有角度敏感性和时变性的散射起伏.本研究为弹道中段碎片诱饵的特性分析与反导效能评估提供了一种可行的数字仿真方案.
Debris clouds generated by ballistic missiles in the midcourse phase pose a significant challenge to target recognition for anti-missile systems.To effectively evaluate the radar scattering characteristics of these debris decoys,this paper proposes an integrated simulation method that combines geometric discretization,dynamics evolution,and Electromagnetic scattering.The method first discretizes the missile shell structure into triangular facets.Subsequently,it combines an improved Gurney initial velocity model with dynamics iteration based on Rodrigues'rotation transformation to simulate the spatio-temporal evolution process of the debris cloud after explosion.The fast iterative shooting and bouncing ray method is employed to calculate the electromagnetic scattering of the time-varying quasi-static debris cloud model on this basis.The simulation analyzes the time-varying characteristics of the radar cross section,the energy diffusion features of the High-Resolution Range Profile,and the angular scattering characteristics of the debris cloud at different grazing angles.The results show that the proposed model can effectively simulate the diffusion process of the debris and its complex scattering fluctuations,which are sensitive to angle and time.This research provides a feasible digital simulation solution for the characteristic analysis of ballistic midcourse debris decoys and the effectiveness evaluation of anti-missile systems.
李丹阳;何宇洁;孙昭;吴迪龙;左炎春;刘伟;王蕊
西安电子科技大学,西安 710071西安电子科技大学,西安 710071西安电子科技大学,西安 710071西安电子科技大学,西安 710071西安电子科技大学,西安 710071西安电子科技大学,西安 710071西安电子科技大学,西安 710071
航空航天
碎片诱饵动力学建模电磁散射弹跳射线法
debris decoydynamics modelingelectromagnetic scatteringshooting and bouncing ray
《空间电子技术》 2026 (2)
111-118,8
国家自然科学基金项目(编号:62301402)
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