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Real-Time Vision-Based Pose Tracking of Spacecraft in Close Range Using Geometric Curve Fitting

机译:基于实时视觉的航天器在近距离使用几何曲线拟合的姿势跟踪

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摘要

This article presents a new framework of real-time vision-based pose tracking for spacecraft in close range using geometric fitting of the imaged geometric primitives (GPs) on the spacecraft. At the first time instant, the tracking is initialized with the template-based pose retrieval and GP-based pose determination. At each subsequent time instant, with the pose prediction from the extended Kalman filter (EKF) as initial value, the GPs are associated with the corresponding image data, and thereby the maximum-likelihood estimation (MLE) for spacecraft pose can be obtained in real time by geometrically fitting the GP projections over the corresponding image data with generalized expectation-maximization and M-estimation. Using the MLE, the EKF generates the final pose estimation and predicts the pose at the next time instant. The basic configurations of the GPs are investigated for the stability of tracking. Sufficient experiments validate the accuracy and the real-time performance of the proposed method.
机译:本文介绍了在航天器上的成像几何基元(GPS)的几何拟合在近距离的近距离航天器的基于航天器的基于航天器的基于航天器的姿势跟踪的新框架。在第一次即时,通过基于模板的姿势检索和基于GP的姿势确定来初始化跟踪。在每个后续时间瞬间,利用从扩展卡尔曼滤波器(EKF)作为初始值的姿态预测,GPS与相应的图像数据相关联,从而可以在实际中获得用于航天器姿势的最大似然估计(MLE)通过通过广义期望最大化和M估计在相应的图像数据上几何地拟合GP投影的时间。使用MLE,EKF生成最终的姿势估计并在下次即时预测姿势。研究了GPS的基本配置,以实现跟踪的稳定性。足够的实验验证了所提出的方法的准确性和实时性能。

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