基于截断混合高斯模型的火箭HRRP重构和飞行姿态估计

    Reconstruction and Flight Attitude Estimation of Rocket HRRP Based on Truncated Mixture of Gaussians Model

    • 摘要: 随着商业航天的蓬勃发展,基于外测数据的火箭飞行姿态估计需求愈发迫切。本文在深入研究火箭高分辨距离像(HRRP)特性的基础上,基于参数化表征思想,采用截断混合高斯模型完成了火箭HRRP重构,实现了有模板库和无模板库2种状态下的火箭飞行姿态估计。采用仿真HRRP序列和飞行HRRP序列测试表明,重构HRRP序列具有信噪比高和稳定性强的优点,采用多包络检测、距离模板匹配和长度投影等方法,稳定实现了基于HRRP数据的火箭飞行分离检测和姿态估计。

       

      Abstract: With the rapid development of commercial spaceflight, the demand for rocket flight attitude estimation based on external measurement data is becoming increasingly urgent. This paper, based on an in-depth study of the characteristics of High-Resolution Range Profiles (HRRP) of rockets, employs a truncated mixed Gaussian model based on the idea of parametric representation to complete the reconstruction of rocket HRRP. This approach achieves rocket flight attitude estimation under two conditions: with and without a template library. Tests using simulated HRRP sequences and actual flight HRRP sequences demonstrate that the reconstructed HRRP sequences have the advantages of high signal-to-noise ratio and strong stability. By employing methods such as multi-envelope detection, range template matching, and length projection, stable implementation of rocket flight separation detection and attitude estimation based on HRRP data is achieved.
       

       

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