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A new stochastic impressionistic low Earth model of the space debris scenario

机译:一种新的空间印象场景的随机印象派低地球模型

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A new Stochastic IMPressionistic Low Earth (SIMPLE) model of the space debris environment using a stochastic approach is presented in this paper. The present approach and philosophy are similar to that utilized for evolving the international standard or other reference atmospheres. Presently, this model describes the debris scenario up to an altitude of 2000 km and with eccentricity less than 0.2 thus covering about 75% of the large space debris objects catalogued in USSPACECOM two line element (TLE) sets. Two types of models one called 'gross' provides insight into the physical process by characterizing the distribution of the number density 'n', eccentricity 'e', and the ballistic coefficient 'B' of objects over the whole of the LEO region for all inclinations put together as also separately. The other called 'local' model characterizes the distribution of 'e' and 'B' of the debris across suitable local altitude and perigee bins useful for mission analysis and risk assessment for spacecraft designers interested in specific altitude or perigee height bins and inclination bands. The number density 'n' in all the gross models can be represented in terms of a mixture of Laplace distributions. The SIMPLE model with much less parameters than in ORDEM96 captures closely all the peak fragment densities without loss of accuracy at other altitudes. The distribution of 'e' and the 'B' in each and every gross and local model can be represented by suitable lognormal distributions. Qualitatively the parameters of the 'n' and 'e' distributions in the gross and the local models exhibit statistically quasi-equilibrium state (though quantitatively the fragment density is varying all over) across the time period from 1999 to 2002 and hence an average is recommended as the model value. Since, the parameters of 'B' show large variations or trend in their values derived from the TLE data sets, the latest year 2002 value is suggested as a reference in the model. Lastly some application areas of the SIMPLE model are provided along with possible approaches to estimate the spatial density of debris objects and their flux in each altitude bin of interest.
机译:本文提出了一种使用随机方法的空间碎片环境的随机随机低地球模型(SIMPLE)。当前的方法和理念类似于用于发展国际标准或其他参考氛围的方法和理念。目前,该模型描述了高达2000 km的高空碎片情况,并且偏心率小于0.2,因此覆盖了USSPACECOM两行元素(TLE)集中分类的大空间碎片对象的75%。两种类型的模型(称为“总”)通过表征物体在整个LEO区域内的数密度“ n”,偏心率“ e”和弹道系数“ B”的分布来提供对物理过程的洞察力倾斜度也分开放置。另一个称为“局部”模型的特征是碎片在适当的局部高度和近地点箱中的分布“ e”和“ B”,这对对特定高度或近地点高度箱和倾角带感兴趣的航天器设计者的任务分析和风险评估非常有用。所有总体模型中的数字密度“ n”可以用拉普拉斯分布的混合表示。与ORDEM96中参数相比,具有更少参数的SIMPLE模型可以紧密捕获所有峰碎片密度,而不会损失其他高度的准确性。每个和每个总体模型和局部模型中“ e”和“ B”的分布都可以用合适的对数正态分布表示。定性地,在1999年至2002年的整个时间段内,总模型和局部模型中“ n”和“ e”分布的参数呈现出统计上的准平衡状态(尽管片段密度在数量上都在变化)。建议作为模型值。由于“ B”的参数在从TLE数据集中得出的值中显示出较大的变化或趋势,因此建议在模型中使用2002年的最新值作为参考。最后,提供了SIMPLE模型的一些应用领域以及可能的方法,以估计碎片物体的空间密度及其在每个目标海拔区域中的通量。

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