Experimental Assessment of a Visual-Laser Relative Navigation Module for CubeSats

Giuseppe Napolano, Claudio Vela, A. Nocerino, R. Opromolla, M. Grassi, Salvatore Amoruso, G. Donfrancesco
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Abstract

This paper presents the Hardware-In-The-Loop testing of a multi-sensor relative navigation module enabling close-proximity operations toward passively cooperative space targets in the frame of On-Orbit Servicing missions. The module, which is designed according to the CubeSat standard to occupy two CubeSat units, consists of a monocular camera and a wide-field-of-view laser range finder, and exploits a sensor fusion logic to provide relative position and attitude (pose) estimates. A laboratory setup is conceived and realized to characterize the pose estimation performance of the module by providing a highly accurate benchmark. Experimental tests show that the module is able to measure its relative position and attitude with respect to a target at operative distances below 2 meters with millimeter and tenths-of-degree level accuracy, respectively. Further tests on a larger-scale trajectory in an uncontrolled environment (in terms of illumination conditions and reference pose solution) demonstrate the capability to perform pose estimation up to operative distances of about 9 meters from the target, keeping reprojection errors at sub-centimeter level, and collecting reliable range finder measurements up to 30 m.
立方体卫星视觉激光相对导航模块的实验评估
本文介绍了一种多传感器相对导航模块的硬件在环测试,该模块能够在在轨服务任务框架下对被动合作空间目标进行近距离操作。该模块根据CubeSat标准设计,占用两个CubeSat单元,由一个单目摄像机和一个宽视场激光测距仪组成,并利用传感器融合逻辑提供相对位置和姿态(姿态)估计。设计并实现了一个实验室设置,通过提供高精度基准来表征模块的姿态估计性能。实验测试表明,该模块能够在2米以下的操作距离内测量其相对位置和相对姿态,精度分别为毫米级和十分度级。在不受控制的环境中(在照明条件和参考姿态解决方案方面)对更大规模的轨迹进行的进一步测试表明,该系统能够在距离目标约9米的操作距离内进行姿态估计,将重投影误差保持在亚厘米级别,并收集可靠的测距仪测量值,最远可达30米。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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