助推段加速度估计

E.L. Crosson, J. B. Romine, D. Willner, S.J. Kusiak
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引用次数: 11

摘要

当只使用公制雷达数据(距离和角度)时,描述火箭飞行的助推阶段是具有挑战性的。结合距离加速度测量结果优越的跟踪性能和大大提高了助推段飞行的特性。本文论述了如何根据目标反射雷达信号的幅值和相位可靠地估计距离加速度。相位导出的距离-加速度估计可用于调整跟踪滤波器,并可合并到滤波器中以改进轨迹重建。距离加速度测量也可用于多目标环境中识别助推目标。这些技术已成功应用于实际火箭发射数据,提高了发射后跟踪和目标识别性能。
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Boost-phase acceleration estimation
Characterizing the boost phase of a rocket's flight is challenging when only metric radar data (range and angles) are used. Incorporating range-acceleration measurements results in superior tracking performance and much improved characterization of boost-phase flight. This paper demonstrates how to estimate range acceleration reliably from the amplitude and phase of the target-reflected radar signal. Phase-derived range-acceleration estimates can be used to tune a tracking filter and can be incorporated into the filter for improved trajectory reconstruction. Range-acceleration measurements can also be used in a multitarget environment to identify boosting targets. These techniques have been used successfully on actual rocket-launch data to improve postmission tracking and object identification performance.
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