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首页> 外文期刊>IEEE Transactions on Aerospace and Electronic Systems >3-D track initiation in clutter using 2-D radar measurements
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3-D track initiation in clutter using 2-D radar measurements

机译:使用2-D雷达测量的杂波3-D轨道启动

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We present an algorithm for initiating 3-D tracks using range and azimuth (bearing) measurements from a 2-D radar on a moving platform. The work is motivated by the need to track possibly low-flying targets, e.g., cruise missiles, using reports from an aircraft-based surveillance radar. Previous work on this problem considered simple linear motion in a flat Earth coordinate frame. Our research extends this to a more realistic scenario where the Earth's curvature is also considered. The target is assumed to be moving along a great circle at a constant altitude. After the necessary coordinate transformations, the measurements are nonlinear functions of the target state and the observability of target altitude is severely limited. The observability, quantified by the Cramer-Rao lower bound (CRLB), is very sensitive to the sensor-to-target geometry. The paper presents a Maximum Likelihood (ML) estimator for estimating the target motion parameters in the Earth-centered Earth-fixed (ECEF) coordinate frame from 2-D range and angle measurements. In order to handle the possibility of false measurements and missed detections, which was not considered previously, we use the Probabilistic Data Association (PDA) algorithm to weight the detections in a frame. The PDA-based modified global likelihood is optimized using a numerical search. The accuracies obtained by the resulting ML-PDA estimator are quantified using the CRLB for different sensor-target configurations. It is shown that the proposed estimator is efficient, that is, it meets the CRLB. Of particular interest is the achievable accuracy for estimating the target altitude, which is not observed directly by the 2-D radar, but can be only inferred from the range and bearing observations.
机译:我们介绍了一种算法,用于使用来自移动平台上的2-D雷达的范围和方位角(轴承)测量来启动3-D轨道。这项工作是由于需要跟踪可能的低飞行目标,例如巡航导弹,使用来自基于飞机的监视雷达的报告。以前的解决问题在平坦的地球坐标框架中被认为是简单的线性运动。我们的研究将此扩展到了一个更现实的情景,其中也考虑了地球的曲率。假设目标沿着恒定的高度沿着大圆圈移动。在必要的坐标变换之后,测量是目标状态的非线性功能,并且目标高度的可观察性严重限制。由Cramer-Rao下限(CRLB)量化的可观察性对传感器到目标几何非常敏感。本文提出了最大似然(ML)估计器,用于估计从2-D范围和角度测量的地球固定的地球固定(ECEF)坐标帧中的目标运动参数。为了处理错误测量和未错过的检测的可能性,未经过先前考虑,我们使用概率数据关联(PDA)算法在帧中重量检测。使用数值搜索优化基于PDA的修改的全局可能性。通过用于不同的传感器目标配置的CRLB来定量由所得ML-PDA估计器获得的精度。结果表明,所提出的估计器是有效的,即,它符合CRLB。特别感兴趣的是估计目标高度的可实现的准确性,其未直接观察到的2-D雷达,但只能从范围和轴承观察中推断出来。

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