基于小波多分辨率分析的弹道导弹助推相位加速度重建

Colter Long, Soundararajan Ezekiel, Larry Pearlstein, J. Raquepas
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引用次数: 0

摘要

近年来,导弹助推段飞行的噪声水平相对于兴趣量而言是非常大的,因此精确表征助推段的飞行特性成为一个非常具有挑战性和突出的研究课题。基于状态观测重建弹道导弹助推段加速剖面是技术情报界、弹道导弹防御界和导弹预警界感兴趣的问题。如果噪声水平不是太大,有一些可用的方法,如吉洪诺夫正则化。然而,如果噪声环境非常高,大多数算法将表现不佳。在本文中,我们探讨了利用小波技术从非常嘈杂的导弹位置随时间的估计中估计导弹推力的问题。探讨了几种小波基函数和多分辨率方法来最有效地解决这一问题。这些技术过去已经成功地用于实际的火箭发射数据。我们的方法可以应用于美国助推段导弹防御,例如保护美国本土免受核攻击,其他大规模杀伤性武器或常规弹道导弹攻击,军事基地,保护美国盟友和合作伙伴。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Ballistic Missile Boost Phase Acceleration Reconstruction using Wavelet Multi-resolution Analysis
In recent years, the accurate characterization of the boost phase of a missile's flight has become a more challenging and prominent research topic as the noise level is extremely large relative to the quantity of interest. Reconstructing the boost phase acceleration profile of a ballistic missile from state observation is of interest to the technical intelligence community, ballistic missile defense, as well as the missile warning community. There are methods available such as Tikhonov regularization if the noise level is not too large. However, if the noise environment is very high most algorithms will perform poorly. In this paper, we explore the problem of estimating the thrust of a missile from very noisy estimates of its position over time by using wavelet techniques. Several wavelet basis functions and multi-resolution methods are explored to yield the most effective solution to this problem. These techniques have been successfully used on actual rocket-launch data in the past. Our method can be applied to US boost-phase missile defense such as protection of US homeland against nuclear attacks, other weapons of mass destructions or conventional ballistic missile attacks, military bases, and protecting US allies and partners.
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