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基于视觉的硬件在环导航设施 TinyV3RSE。

The TinyV3RSE Hardware-in-the-Loop Vision-Based Navigation Facility.

机构信息

Department of Aerospace Science and Technology, Politecnico di Milano, Via Giuseppe La Masa, 34, 20156 Milano, Italy.

出版信息

Sensors (Basel). 2022 Nov 30;22(23):9333. doi: 10.3390/s22239333.

Abstract

The increase in number of interplanetary probes has emphasized the need for spacecraft autonomy to reduce overall mission costs and to enable riskier operations without ground support. The perception of the external environment is a critical task for autonomous probes, being fundamental for both motion planning and actuation. Perception is often achieved using navigation sensors which provide measurements of the external environment. For space exploration purposes, cameras are among the sensors that provide navigation information with few constraints at the spacecraft system level. Image processing and vision-based navigation algorithms are exploited to extract information about the external environment and the probe's position within it from images. It is thus crucial to have the capability to generate realistic image datasets to design, validate, and test autonomous algorithms. This goal is achieved with high-fidelity rendering engines and with hardware-in-the-loop simulations. This work focuses on the latter by presenting a facility developed and used at the Deep-space Astrodynamics Research and Technology (DART) Laboratory at Politecnico di Milano. First, the facility design relationships are established to select hardware components. The critical design parameters of the camera, lens system, and screen are identified and analytical relationships are developed among these parameters. Second, the performances achievable with the chosen components are analytically and numerically studied in terms of geometrical accuracy and optical distortions. Third, the calibration procedures compensating for hardware misalignment and errors are defined. Their performances are evaluated in a laboratory experiment to display the calibration quality. Finally, the facility applicability is demonstrated by testing imageprocessing algorithms for space exploration scenarios.

摘要

随着星际探测器数量的增加,人们越来越强调航天器自主性的必要性,以降低整体任务成本,并使风险操作能够在没有地面支持的情况下进行。外部环境感知是自主探测器的一项关键任务,对于运动规划和执行都至关重要。环境感知通常使用导航传感器来实现,这些传感器提供外部环境的测量值。对于太空探索目的,相机是在航天器系统级别提供导航信息的传感器之一,其约束条件较少。图像处理和基于视觉的导航算法被用于从图像中提取有关外部环境和探测器在其中位置的信息。因此,具有生成逼真图像数据集的能力对于设计、验证和测试自主算法至关重要。这一目标可以通过高保真度渲染引擎和硬件在环仿真来实现。这项工作侧重于后者,介绍了在米兰理工大学深空动力学研究和技术 (DART) 实验室开发和使用的一种设施。首先,建立了设施设计关系,以选择硬件组件。确定了相机、镜头系统和屏幕的关键设计参数,并在这些参数之间开发了分析关系。其次,从几何精度和光学变形的角度,对所选组件的性能进行了分析和数值研究。第三,定义了补偿硬件不对准和误差的校准程序。在实验室实验中评估了它们的性能,以显示校准质量。最后,通过测试用于太空探索场景的图像处理算法,展示了该设施的适用性。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/4992/9740262/39e9c4fbde20/sensors-22-09333-g001.jpg

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