Detection of changes in the motion of Earth-orbiting objects by autoregressive models in conditions of non-equidistant observations

O. Sarychev
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Abstract

The problem of increasing prediction accuracy for the motion of Earth-orbiting objects (EOOs) and detecting changes therein is topical for the tasks of spacecraft life prediction, space debris cataloguing, and navigation. Therefore, the problem of detecting changes in dynamic systems characterized by non-equidistant observations is topical. The purpose of this work is the development of autoregressive models with observations non-equidistant in time to detect changes in EOO motion. The methods employed are multivariate statistical analysis, time series prediction, and complex-system simulation under structural uncertainty. Data generated by NORAD (USA) were used as initial observations to describe EOO motion. They are actual, constantly updated, and freely available via the Internet. These data are presented in the Two-Line Element (TLE) format, which is a data format encoding a list of orbital elements of an EOO for a given point in time. This paper presents a method for constructing autoregressive models to describe the dynamics of EOOs represented by time series of TLE elements with values non-equidistant in time. On its basis, autoregressive models of the Sich-2 spacecraft’s dynamics were constructed. The standard errors of the models were analysed on examination samples, and significant deviations of the standard errors for the basic variables (apogee, perigee, eccentricity, longitude of ascending node, perigee argument, and average anomaly) were found, thus demonstrating changes in the Sich-2 motion from its basic regime. The novelty of this work lies in that the problem of detecting changes in EOO motion characteristics based on the proposed type of autoregressive models has not been considered before. Its practical value lies in that the simulation of the Sich-2 motion using time series of TLE elements allows one to detect changes in motion regimes; the method may be used in detecting in-service changes in EOO properties.
在非等距观测条件下用自回归模型检测地球轨道物体运动的变化
提高对地球轨道物体运动的预测精度并检测其变化是航天器寿命预测、空间碎片编目和导航任务中的一个热点问题。因此,检测以非等距观测为特征的动态系统变化的问题是当前的热点问题。这项工作的目的是发展具有非等距观测时间的自回归模型,以检测EOO运动的变化。采用多元统计分析、时间序列预测和结构不确定性下的复杂系统模拟等方法。由NORAD(美国)生成的数据被用作描述EOO运动的初始观测数据。它们是真实的,不断更新的,并且可以通过互联网免费获得。这些数据以双线元(TLE)格式呈现,这是一种编码给定时间点EOO轨道元素列表的数据格式。本文提出了一种构造自回归模型的方法来描述由时间上非等距的TLE元素时间序列所表示的eoo动态。在此基础上,建立了神舟二号航天器动力学的自回归模型。在检验样本上分析了模型的标准误差,发现远地点、近地点、离心率、升交点经度、近地点角和平均异常等基本变量的标准误差出现了显著偏差,从而表明了星宿2号的运动与基本状态的变化。这项工作的新颖之处在于,基于所提出的自回归模型类型检测EOO运动特征变化的问题以前没有考虑过。它的实用价值在于,利用TLE元素的时间序列模拟sch -2运动,可以检测运动状态的变化;该方法可用于检测使用中EOO属性的变化。
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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