Determination of the force exerted by an ion beam on a space debris object from the edges of its images using deep learning

M. Redka
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Abstract

The goal of this article is to develop an effective image preprocessing algorithm and a neural network model for determining the force to be transmitted to a space debris object (SDO) for its non-contact deorbit. In the development and study of the algorithm, use was made of methods of theoretical mechanics, machine learning, computer vision, and computer simulation. The force is determined using a photo taken by an onboard camera. To increase the efficiency of the neural network, an algorithm was developed for feature recognition by the SDO edge in the photo. The algorithm, on the one hand, selects a sufficient number of features to describe the properties of the figure and, on the other hand, significantly reduces the amount of data at the neural network input. A dataset with the features and corresponding reference force values was created for model training. A neural network model was developed to determine the force to be exerted on a SDO from the SDO features. The model was tested using a set of eighteen calculated cases to determine the effectiveness, accuracy, and speed of the algorithm. The proposed algorithm was compared with two existing ones: the method of central projections onto an auxiliary plane and the multilayered neural network model that calculates the force using the SDO orientation parameters. The comparison was performed using the root mean square error, the maximum absolute error, and the maximum relative error. The test results are presented as tables and graphs. The proposed approach makes it possible to develop a system of SDO non-contact removal that does not need to determine the exact relative position and orientation with respect to the active spacecraft. Instead, the algorithm uses camera-taken photos, from which the features necessary for calculation are extracted. This makes it possible to reduce the requirements for its computing elements, to abandon sensors for determining the relative position and orientation, and to reduce the cost of the system.
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利用深度学习从图像边缘确定离子束对空间碎片物体施加的力
本文的目标是开发一种有效的图像预处理算法和神经网络模型,以确定传输到空间碎片物体(SDO)以使其非接触脱离轨道的力。在算法的开发和研究中,使用了理论力学、机器学习、计算机视觉和计算机仿真等方法。力是通过机载相机拍摄的照片确定的。为了提高神经网络的效率,提出了一种利用照片中的SDO边缘进行特征识别的算法。该算法一方面选择了足够数量的特征来描述图的属性,另一方面显著减少了神经网络输入的数据量。创建具有特征和相应参考力值的数据集用于模型训练。开发了一个神经网络模型来根据SDO特征确定要施加在SDO上的力。用一组18个计算案例对模型进行了测试,以确定算法的有效性、准确性和速度。将该算法与已有的辅助平面中心投影法和利用SDO方向参数计算力的多层神经网络模型进行了比较。采用均方根误差、最大绝对误差和最大相对误差进行比较。试验结果以图表形式呈现。所提出的方法使开发SDO非接触移除系统成为可能,该系统不需要确定相对于活动航天器的确切相对位置和方向。相反,该算法使用相机拍摄的照片,从中提取计算所需的特征。这使得减少对其计算元件的要求,放弃用于确定相对位置和方向的传感器,并降低系统的成本成为可能。
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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