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Estimability of Thrusting Trajectories in 3-D from a Single Passive Sensor with Unknown Launch Point

机译:具有未知发射点的单个无源传感器在3-D中推力轨迹的可估计性

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The problem of estimating the state of thrusting/ballistic endoatmospheric projectiles moving in 3-dimensional (3-D) space using 2-dimensional (2-D) measurements from a single passive sensor is investigated. In this study, the location information of projectile's launch point (LP) is unavailable and this could significantly affect the performance of the estimation and the IPP. The LP altitude is then an unknown target parameter. The estimability is analyzed based on the Fisher Information Matrix (FIM) of the target parameter vector, comprising the initial launch (azimuth and elevation) angles, drag coefficient, thrust and the LP altitude, which determine the trajectory according to a nonlinear motion equation. The full rank of the FIM ensures that one has an estimable target parameters. The corresponding Cramer-Rao lower bound (CRLB) quantifies the estimation performance of the estimator that is statistically efficient and can be used for IPP. In view of the inherent nonlinearity of the problem, the maximum likelihood (ML) estimate of the target parameter vector is to be sought by using a mixed (partially grid-based) search approach. For a selected grid in the drag-coefficient-thrust-altitude subspace, the proposed parallelizable approach is shown to have reliable estimation performance and further leads to the final IPP of high accuracy.
机译:研究了使用来自单个无源传感器的二维(2-D)测量的三维(3-D)空间在三维(3-D)空间中移动的推动/弹道型腔内射弹的问题进行了研究。在这项研究中,射弹发射点(LP)的位置信息不可用,这可能会显着影响估计和IPP的性能。 LP高度是一个未知的目标参数。基于目标参数向量的Fisher信息矩阵(FIM)来分析可评估性,包括根据非线性运动方程确定轨迹的初始发射(方位角和高度)角度,拖动系数,推力和LP高度。 FIM的全部等级可确保一个具有可估计的目标参数。相应的Cramer-Rao下限(CRLB)量化了统计学高效的估计性能,可用于IPP。鉴于问题的固有非线性,通过使用混合(部分网格的)搜索方法寻求目标参数向量的最大似然(ML)估计。对于拖动系数推力 - 高度子空间中的选定网格,所提出的并行方法被示出具有可靠的估计性能,并进一步导致最终的高精度IPP。

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