空间碎片:建模和可探测性

C. Wiedemann, J. Lorenz, J. Radtke, C. Kebschull, A. Horstmann, E. Stoll
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引用次数: 1

摘要

探测和清除空间碎片需要高精度的轨道确定。了解轨道上碎片物体的分布情况对于主动或被动传感器确定轨道是必要的。这些结果可以用来研究轨道,在轨道上可以找到一定大小、一定频率的物体。根据传感器性能模型了解目标的轨道分布及其特性,为估计期望的检测率提供了依据。为此,需要对空间碎片环境进行综合建模。本文概述了空间碎片环境知识的现状。特别是对未编目的小对象进行评估。此外,还讨论了有关更新当前空间碎片模型的改进问题。空间碎片环境模型是基于对历史事件的模拟,比如在地球轨道上实际发生的爆炸和碰撞造成的碎片。考虑到所有的扰动力,通过传播轨道来模拟碎片的轨道分布直到一个参考历元。将建模的目标总体与实测数据进行比较并验证。该模型根据空间物体的大小和数量提供了空间物体的统计分布。这种分布是基于对轨道力学的正确考虑。这样就可以对空间碎片环境进行真实的描述。随后,就可以提供一个现实的预测,即在某些轨道上预计会有多少碎片。为了验证该模型,开发了一种软件工具,可以模拟地基或天基传感器的观测行为。因此,可以将公布的测量数据结果与模拟检测结果进行比较。此工具也可用于传感器测量活动的模拟。因此,有可能对未编目的空间碎片的探测率作出估计。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Space debris: modeling and detectability
High precision orbit determination is required for the detection and removal of space debris. Knowledge of the distribution of debris objects in orbit is necessary for orbit determination by active or passive sensors. The results can be used to investigate the orbits on which objects of a certain size at a certain frequency can be found. The knowledge of the orbital distribution of the objects as well as their properties in accordance with sensor performance models provide the basis for estimating the expected detection rates. Comprehensive modeling of the space debris environment is required for this. This paper provides an overview of the current state of knowledge about the space debris environment. In particular non-cataloged small objects are evaluated. Furthermore, improvements concerning the update of the current space debris model are addressed. The model of the space debris environment is based on the simulation of historical events, such as fragmentations due to explosions and collisions that actually occurred in Earth orbits. The orbital distribution of debris is simulated by propagating the orbits considering all perturbing forces up to a reference epoch. The modeled object population is compared with measured data and validated. The model provides a statistical distribution of space objects, according to their size and number. This distribution is based on the correct consideration of orbital mechanics. This allows for a realistic description of the space debris environment. Subsequently, a realistic prediction can be provided concerning the question, how many pieces of debris can be expected on certain orbits. To validate the model, a software tool has been developed which allows the simulation of the observation behavior of ground-based or space-based sensors. Thus, it is possible to compare the results of published measurement data with simulated detections. This tool can also be used for the simulation of sensor measurement campaigns. It is therefore possible to provide an estimation of the detection rates of the non-cataloged population of space debris.
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